+ All Categories
Transcript
  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    1/249

    SCHEME AND SYLLABI

    FOR

    THIRD TO EIGHTH SEMESTERS

    OF

    BACHELOR OF TECHNOLOGY

    IN

    AERONAUTICAL ENGINEERING

    FROM 2009 ADMISSION ONWARDS

    CALICUT UNIVERSITY (P.O), THENHIPALAM

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    2/249

    B.TECH. AERONAUTICAL ENGINEERING

    CURRICULAM

    2009 Admission onwards

    Combined First and Second Semesters (Common for all branches)

    Code Subject

    Hours per week Marks

    L T P/D InternalSemEnd

    SemEnd

    duration-

    hours

    Credits

    EN08 101 Engineering Mathematics I 2 1 - 30 70 3 4

    EN08 102 Engineering Mathematics II 2 1 - 30 70 3 4

    EN08 103 Engineering Physics 2 - 30 70 3 3

    EN08103(P)

    Physics Lab - - 1 50 50 3 1

    EN08 104 Engineering Chemistry 2 - 30 70 3 3

    EN08

    104(P)Chemistry Lab - - 1 50 50 3 1

    EN08 105 Engineering Mechanics 2 1 - 30 70 3 4

    EN08 106 Basics of Civil & Mechanical Engg. 2 1 - 30 70 3 4

    EN08 107Basics of Electrical, Electronics and

    Communication Engg.2 1 - 30 70 3 4

    EN08 108 Engineering Graphics 0 - 3 30 70 3 3

    EN08

    109(P) Computer Programming in C 1 - 1 50 50 3 3EN08

    110A(P)Mechanical Workshop - - 2 50 50 3 2

    EN08110B(P)

    Electrical and Civil Workshops - - 2 50 50 3 2

    TOTAL 15 5 10 38

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    3/249

    Third Semester - Aeronautical Engineering

    Code Subject

    Hours per week Marks

    L T P/D Internal

    Sem

    End

    SemEnd

    duration-hours

    Credits

    EN09 301A Engineering Maths III 3 1 - 30 70 3 4

    EN09 302 Humanities and Social Science 2 1 - 30 70 3 3

    AN09 303Fluid Mechanics and HydraulicMachinery

    4 1 - 30 70 3 5

    ANO9 304Computer Assisted MachineDrawing

    1 - 3 30 70 3 4

    AN09 305 Electrical Technology 3 1 - 30 70 3 4

    AN09 306 Metallurgy and Material Science 3 1 - 30 70 3 4

    AN09

    307(P)

    Electrical Engineering Lab - - 3 50 50 3 2

    AN09(P)308

    Production engineering Lab - - 3 50 50 3 2

    TOTAL 16 5 9 28

    Fourth Semester - Aeronautical Engineering

    Code Subject

    Hours per week Marks

    L T P/D Internal SemEnd

    Sem

    Endduration-hours

    Credits

    EN09 401A Engineering Maths IV 3 1 - 30 70 3 4

    EN09 402 Environmental Science 2 1 - 30 70 3 3

    AN09 403 Aircraft Structure I 4 1 - 30 70 3 5

    AN09 404 Heat Transfer 3 1 - 30 70 3 4

    AN09 405 Mechanics of Solids 3 1 - 30 70 3 4

    AN09 406 Elements of Aeronautics 3 1 - 30 70 3 4

    AN09407(P)

    Material Testing Lab - - 3 50 50 3 2

    AN09408(P)

    Aircraft Structure Lab I - - 3 50 50 3 2

    TOTAL 18 6 6 28

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    4/249

    Fifth Semester - Aeronautical Engineering

    Code Subject

    Hours perweek

    Marks

    L T P/D

    Internal

    SemEnd

    SemEnd

    duration-hours

    Credits

    AN 09 501 Microprocessor & Applications 4 1 - 30 70 3 5

    AN 09 502 Control Engineering 3 1 - 30 70 3 4

    AN 09 503 Numerical Methods 3 1 - 30 70 3 4

    AN 09 504 Flight Dynamics 3 1 - 30 70 3 4

    AN 09 505 Aircraft Structure II 3 1 - 30 70 3 4

    AN 09 506 Aerodynamics I 2 1 - 30 70 3 3

    AN 09 507(P) Aircraft Structures lab II - - 3 50 50 3 2

    AN 09 508(P)Aircraft Structures Repairs andMaintenance Lab

    - - 3 50 50 3 2

    TOTAL 18 6 6 28

    Sixth Semester - Aeronautical Engineering

    Code SUBJECT

    Hours per week Marks

    L T P/D InternalSemEnd

    Sem Endduration-

    hoursCredits

    AN 09 601 Propulsion I 4 1 - 30 70 3 5

    AN 09 602

    Aircraft systems,Instrumentationand applications

    3 1 - 30 70 3 4

    AN 09 603 Experimental stress analysis 3 1 - 30 70 3 4

    AN 09 604 Aero Dynamics II 3 1 - 30 70 3 4

    AN 09 605 Computer Integrated Manufacturing 2 1 - 30 70 3 3

    AN09 606 Elective - I 3 1 - 30 70 3 4

    AN 09607(P) Mini Project / Lab

    - - 3 50 50 3 2

    AN09 608(P) Aerodynamics Lab - - 3 50 50 3 2

    TOTAL 18 6 6 28

    ELECTIVES:

    AN09 L01 Composite Materials

    AN09 L02 Computational Methods in Engineering

    AN09 L03 Industrial Maintenance

    AN09 L04 Quality Engineering and Management

    AN09 L05 Tool Engineering and Design

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    5/249

    Seventh Semester - Aeronautical Engineering

    Code Subject

    Hours per week Marks

    L T P/D InternalSem

    End

    Sem Endduration-

    hours

    Credits

    AN09 701 Propulsion II 4 1 - 30 70 3 5

    AN 09 702 Avionics 3 1 - 30 70 3 4

    AN 09 703 Workshop Technology 2 1 - 30 70 3 3

    AN 09 704Computational FluidDynamics

    2 1 - 30 70 3 3

    AN 09 705 Elective - II 3 1 - 30 70 3 4

    AN 09 706 Elective - III 3 1 - 30 70 3 4

    AN 09 707(P) Avionics Lab - - 3 50 50 3 2

    AN 09 708(P) Propulsion Lab - - 3 50 50 3 2

    AN09 709(P) Project - - 1 100 - - 1

    TOTAL 17 6 7 28

    Eighth Semester - Aeronautical Engineering

    Code Subject

    Hours per week Marks

    L T P/D InternalSem

    End

    Sem Endduration-

    hoursCredits

    AN09 801Reliability Engineering

    4 1 - 30 70 3 5

    AN 09 802Air Craft Rules andRegulations C. A. R I and

    II

    2 1 - 30 70 3 3

    AN 09 Lxx Elective - IV 3 1 - 30 70 3 4

    AN 09 Lxx Elective - V 3 1 - 30 70 3 4

    AN 09 805(P) Seminar - - 3 100 - 3 2

    AN 09 806(P) Project - - 11 100 - 3 7

    AN 09 807(P) Viva Voce - - - 100 - 3 3

    TOTAL 12 4 14 28

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    6/249

    ELECTIVES (Seventh and Eighth Semester):

    AN09 L06 Theory of Elasticity

    AN09 L07 Space Mechanics

    AN09 L08 Aero Engine Maintenance and Repair

    AN09 L09 Vibration and Aero elasticity

    AN09 L10 Finite Element Method

    AN09 L11 Airframe Maintenance and Repair

    AN09 L12 Theory of Plates and Shells

    AN09 L13 Combustion Technology

    AN09 L14 Refrigeration Engineering

    AN09 L15 Helicopter Maintenance

    AN09 L16 Project Management

    AN09 L17 Rocket and Missiles

    AN09 L18 Robotics

    AN09 L19 Turbo Machinery

    AN09 L20 Acoustics and noise control

    AN09 L21 Research Methodology

    AN09 L22 Composite Materials and Structures

    AN09 L23 Mechatronics

    AN09 L24 Wind tunnel Techniques

    AN09 L25 Fatigue and fracture

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    7/249

    GLOBAL ELECTIVES:

    EE09 L25 Robotic and Automation

    ME09 L23 Industrial Safety Engineering

    CE09 L24 Remote Sensing and GIS

    BT09 L24 Bio ethics and Intellectual Property Rights

    CH09 L23 Nano material and Nanotechnology

    CH09 L24 Industrial Pollution control

    EE09 L22 Soft computing

    PE09 L24 Industrial psychology

    PE09 L25 Entrepreneurship

    ME09 L25 Energy Engineering and Management

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    8/249

    THIRD SEMESTER

    EN09 301: Engineering Mathematics III(Common for all branches)

    ObjectiveThis course provides a quick overview of the concepts and results in complex analysis

    that may be useful in engineering. Also it gives an introduction to linear algebra and Fouriertransform which are wealths of ideas and results with wide area of application.

    Module I: Functions of a Complex Variable (13 hours)Functions of a Complex Variable Limit Continuity Derivative of a Complex function Analytic functions Cauchy-Riemann Equations Laplace equation Harmonic Functions

    Conformal Mapping Examples: Z

    n

    , sinz, cosz, sinhz, coshz, (z+

    1

    /Z ) MobiusTransformation.

    Module II: Functions of a Complex Variable (14 hours)Definition of Line integral in the complex plane Cauchys integral theorem (Proof of

    existence of indefinite integral to be omitted) Independence of path Cauchys integralformula Derivatives of analytic functions (Proof not required) Taylor series Laurentseries Singularities and Zeros Residues Residue Integration method Residues andResidue theorem Evaluation of real integrals.

    Module III: Linear Algebra (13 hours) - Proofs not requiredVector spaces Definition, Examples Subspaces Linear Span Linear Independence

    Linear Dependence Basis Dimension Ordered Basis Coordinate Vectors TransitionMatrix Orthogonal and Orthonormal Sets Orthogonal and Orthonormal Basis Gram-Schmidt orthogonolisation process Inner product spaces Examples.

    Module IV: Fourier Transforms (14 hours)Fourier Integral theorem (Proof not required) Fourier Sine and Cosine integralrepresentations Fourier Transforms Fourier Sine and Cosine Transforms Properties ofFourier Transforms.

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial er week

    Text Books

    Module I:

    Erwin Kreysig,Advanced Engineering Mathematics, 8e, John Wiley and Sons, Inc.Sections: 12.3, 12.4, 12.5, 12.6, 12.7, 12.9Module II:Erwin Kreysig,Advanced Engineering Mathematics, 8e, John Wiley and Sons, Inc.Sections: 13.1, 13.2, 13.3, 13.4, 14.4, 15.1, 15.2, 15.3, 15.4Module III:Bernaed Kolman, David R Hill, Introductory Linear Algebra, An Applied First Course, PearsonEducation.

    Sections: 6.1, 6.2, 6.3, 6.4, 6.7, 6.8, Appendix.B.1Module IV:Wylie C.R and L.C. Barrett,Advanced Engineering Mathematics, McGraw Hill.Sections: 9.1, 9.3, 9.5

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    9/249

    Reference Books

    1. H S Kasana, Complex Variables, Theory and Applications, 2e, Prentice Hall ofIndia.

    2. John M Howie, Complex Analysis, Springer International Edition.

    3. Shahnaz bathul, Text book of Engineering Mathematics, Special functions andComplex Variables, Prentice Hall of India.

    4. Gerald Dennis Mahan,Applied mathematics, Springer International Edition.

    5. David Towers, Guide to Linear Algebra, MacMillan Mathematical Guides.6. Howard Anton, Chris Rorres, Elementary Linear Algebra, Applications

    Version, 9e, John Wiley and Sons.

    7. Anthony Croft, Robert Davison, Martin Hargreaves, Engineering Mathematics,3e, Pearson Education.

    8. H Parthasarathy, Engineering Mathematics, A Project & Problem basedapproach, Ane Books India.

    9. B V Ramana,Higher Engineering Mathematics, McGrawHill.

    10. Sarveswara Rao Koneru,Engineering Mathematics, Universities Press.11. J K Sharma, Business Mathematics, Theory and Applications, Ane Books India.12. John bird,Higher Engineering Mathematics, Elsevier, Newnes.

    13. M Chandra Mohan, Vargheese Philip,Engineering Mathematics-Vol. I, II, III &IV., Sanguine Technical Publishers.

    14. N Bali, M Goyal, C Watkins,Advanced Engineering Mathematics, A ComputerApproach, 7e, Infinity Science Press, Fire Wall Media.

    15. V R Lakshmy Gorty,Advanced Engineering Mathematics-Vol. I, II., Ane BooksIndia. Sastry S.S., Advanced Engineering Mathematics-Vol. I and II., PrenticeHall of India.

    16. Lary C Andrews, Bhimsen K Shivamoggi,

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group discussions,

    quiz, literature survey, seminar, term-project, software exercises, etc.10% - Regularity in the class

    University Examination Pattern

    PART A: Short answer questions (one/two sentences) 5 x 2 marks=10 marks

    All questions are compulsory. There should be at least onequestion from each module and not more than two questionsfrom any module.

    PART B Analytical/Problem solving questions 4 x 5 marks=20 marks

    Candidates have to answer four questions out of six. Thereshould be at least one question from each module and not morethan two questions from any module.

    PART C: Descriptive/Analytical/Problem solving questions 4 x 10 marks=40 marks

    Two questions from each module with choice to answer one question.

    Maximum Total Marks: 70

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    10/249

    EN09 302: Humanities and Communication Skills(Common to all branches)

    Objective

    To identify the most critical issues that confronted particular periods and locations in

    history; To identify stages in the development of science and technology;

    to understand the purpose and process of communication;

    to produce documents reflecting different types of communication such as technicaldescriptions, proposals ,and reports;

    To develop a positive attitude and self-confidence in the workplace; and

    To develop appropriate social and business ethics.

    Module I (8 hours)Humanities, Science and Technology: Importance of humanities to technology, education andsociety- Impact of science and technology on the development of modern civilization.Contributions of ancient civilization: Chinese, Indian, Egyptian and Greek.Cultural, Industrial, Transportation and Communication revolutions.Advances in modern India: Achievements in information, communication and spacetechnologies.

    Module II (9 hours)Concept of communication: The speaker/writer and the listener/reader, medium ofcommunication, barriers to communication, accuracy, brevity, clarity and appropriatenessReading comprehension: Reading at various speeds, different kinds of text for differentpurposes, reading between lines.Listening comprehension: Comprehending material delivered at fast speed and spoken

    material, intelligent listening in interviewsSpeaking: Achieving desired clarity and fluency, manipulating paralinguistic features ofspeaking, task oriented, interpersonal, informal and semi formal speaking, making a short

    classroom presentation.Group discussion: Use of persuasive strategies, being polite and firm, handling questions andtaking in criticisms on self, turn-taking strategies and effective intervention, use of bodylanguage.

    Module III (10 hours)Written Communication : Note making and taking, summarizing, notes and memos,developing notes into text, organization of ideas, cohesion and coherence, paragraph writing,ordering information in space and time, description and argument, comparison and contrast,narrating events chronologically. Writing a rough draft, editing, proof reading, final draft andstyling text.Technical report writing: Synopsis writing, formats for reports. Introductory report, Progress

    report, Incident report, Feasibility report, Marketing report, Field report and Laboratory testreport

    Teaching scheme Credits: 32 hours lecture and 1 hour tutorial per week

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    11/249

    Project report: Reference work, General objective, specific objective, introduction, body,illustrations using graphs, tables, charts, diagrams and flow charts. Conclusion and referencesPreparation of leaflets, brochure and C.V.

    Module IV (9 hours)Human relations and Professional ethics: Art of dealing with people, empathy and sympathy,hearing and listening. Tension and stress, Methods to handle stress

    Responsibilities and rights of engineers- collegiality and loyalty Respect for authority Confidentiality conflicts of interest Professional rights, Rights of information, SocialresponsibilitySenses of ethics variety of moral issues Moral dilemma Moral autonomy Attributes ofan ethical personality right action self interest

    Reference Books

    1. Meenakshi Raman and Sangeeta Sharma, Technical Communication- Principles and

    Practice Oxford University press, 20062. Jayashree Suresh and B S Raghavan,Professional Ethics, S Chand and Company Ltd,

    2005

    3. Subrayappa,History of Science in India, National Academy of Science, India4. R C Bhatia, Business Communication, Ane Books Pvt. Ltd, 2009

    5. Sunita Mishra and C Muralikrishna, Communicatin Skils for Engineers, PearsonEducation, 2007.

    6. Jovan van Emden and Lucinda Becker, Effective Communication for Arts andHumanities Students, Palgrave macmillam, 2009

    7. W C Dampier,History of Science, Cambridge University Press8. Vesilind,Engineering, Ethics and the Environment, Cambridge University Press

    9. Larson E,History of Inventions, Thompson Press India Ltd.10. Bernal J.D, Science in History, Penguin Books Ltd11. Encyclopedia Britannica,History of Science, History of Technology

    12. Brownoski J, Science and Human Values, Harper and Row13. Schrodinger, Nature and Greeks and Science and Humanism, Cambridge University

    Press

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group discussions,

    quiz, literature survey, seminar, term-project, software exercises, etc.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    12/249

    University Examination Pattern

    PART A: Short answer questions (one/two sentences) 5 x 2 marks=10 marks

    All questions are compulsory. There should be at least one

    question from each module and not more than two questions

    from any module.

    PART B: Analytical/Problem solving questions 4 x 5 marks=20 marks

    Candidates have to answer four questions out of six. Thereshould be at least one question from each module and not morethan two questions from any module.

    PART C: Descriptive/Analytical/Problem solving questions 4 x 10 marks=40 marks

    Two questions from each module with choice to answer onequestion.

    Maximum Total Marks: 70

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    13/249

    AN09 303 FLUID MECHANICS AND MACHINERY

    Teaching schemeCredits: 5

    4 hours lecture and I hour tutorial per week

    ObjectiveTo understand the structure and properties of fluidTo understand the appreciate the complexities involved in solving the fluid flow problemsTo understand the mathematical techniques already in vogue and apply them to the solutionsof pactical flow problemsTo understand the energy exchange process in fluid mechanics handling incompressible fluids

    Module I (17hours)Properties of fluids-pressure, density, specific gravity, specific weight, viscosity,compressibility, vapor pressure - gas laws - Capillarity and surface tension-various types of

    manometers and pressure gauges-transmission of fluid pressure-continuity equation for one-dimensional steady flow. Bernoulli's equation for steady, one dimensional incompressibleflow- venturimeter-orifice meter -pitot tube-notches-weirs.

    Module II (20hours)Flow of incompressible fluids through pipes - Laminar flow through circular tubes and Annuliboundary layer concepts - Boundary layer thickness - Reynolds experiment-Laws of fluidfriction in laminar flow-steady laminar flow in circular pipes-Haigen-Poissullie law .Darcy

    Weisbach equation-Chezys formula- Friction factor - Moody diagram -transmission of powerthrough pipes- Flow through pipes in series and in parallel - Commercial pipes.Dimensional analysis: Dimensions and units, the Buckingham theorem. Discussions ondimensionless parameters - Models and similitude - Application of dimensionless parameters.

    Module III (18hours)Impact of jets on vanes -flat, curved, stationary and moving vanes-radial flow over vanes-hydraulic turbines-classification - Pelton wheel, Francis turbine and Kaplan turbine-work

    done and efficiency-draft tube-surge tank-penstock-governing-cavitation-specific speed-similarity and model testing-selection of water turbines for power plantsPositive displacement pumps-reciprocating pumps-inertia pressure-air vessels and theirpurpose-separation and cavitation-slip and efficiency-multi-cylinder pumps

    Module IV (17hours)Rotary motion of liquids-free, forced, spiral, and vortex flow, rotodynamic pumps:-centrifugalpumps impeller, casing - manometric heads, work, efficiency and losses-priming-specific

    speed. Performance characteristics-multistage pumps -selection of pumps-pumping devices-Hydraulic ram, jet pumps, gear pumps, vane pump, lobe pump, rotary pumps.

    Reference BooksFluid Mechanics and Machines: R.K.Bansal .Hydraulics and Fluid mechanics: LewittHydraulics and Fluid mechanics: Dr..Jagadish Lal

    Fluid flow machines: N.S.Govinda RaoFluid mechanics and machines : Modi and Seth.Fluid Mechanics (IV th Edn.), J. F. Douglas, Pearson education.Introduction to fluid dynamics, Robert W. Fox, John Wiley and sons

    Theory and applications of fluid mechanics, K. Subrahmanya, (TMH)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    14/249

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group

    discussions, quiz, literature survey, seminar, term-project, software exercises, etc.

    10% - Regularity in the class

    University Examination Pattern

    PART A: Short answer questions (one/two sentences) 5 x 2 marks=10 marks

    All questions are compulsory. There should be at least one

    question from each module and not more than two questionsfrom any module.

    PART B: Analytical/Problem solving questions 4 x 5 marks=20 marks

    Candidates have to answer four questions out of six. There

    should be at least one question from each module and not morethan two questions from any module.

    PART C: Descriptive/Analytical/Problem solving questions 4 x 10 marks=40 marks

    Two questions from each module with choice to answer one question.

    Maximum Total Marks: 70

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    15/249

    AN09 304: Computer Assisted Machine Drawing

    Teaching scheme Credits:4

    3 hours practical and 1 hour theory per week

    Objective : To impart the fundamental concepts of machine drawing.

    To develop primary knowledge of working drawings.

    To produce orthographic drawing of different machine parts.

    To develop skill to produce assembly drawings.

    To develop skill to produce detailed drawings of machines parts from

    assembly drawing.

    To develop skill to produce drawings by using any standard CAD

    software.

    Module I(12 hours - 1 Printout, 2 Drawing sheets)

    a) Joints : Bolted joints using hexagonal, square and stud bolts and nuts :Types of cotters andpins -Sleeve and cotter joints - Strap joint and knucklejoints, Pipe joints : Socket and spigot

    joints Flanged hydraulic joints Union joints, Rivet heads : Types of riveting - Lap and buttjoint Zigzag and chain structure - Boiler joints.

    b) Couplings and pulleys: Types of shaft keys and-their proportions: Solid and split muff

    couplings -Protected and flexible type -Claw coupling - Universal coupling, Pulleys: Flatpulleys - V-pulleys - Stepped cone pulleys.

    Module II (26 Hrs. - 2 Printouts, 4 Drawing sheets)a) Tolerances and Fits - Limits and tolerances of machine parts - Hole system and shaft

    system of tolerances - Designation of fundamental deviation -Types of fits and their selection- Indication of dimensional tolerances and fits on simple machine parts - Geometricaltolerances - Recommended symbols - Indication of geometrical tolerances on simple machine

    parts - Surface roughness - Indication of surface finish on drawings - Preparation of shopfloor drawings of simple machine parts.

    b) Bearings - Solid journal bearings - Bushed bearings - Plummer block and footstep bearings-Types of rolling contact bearings -Conventional representation of ball and roller bearings -Assembly of radial and thrust type rolling contact bearings in housing. (Scaled drawings ofmachine parts or their assembly showing dimensional tolerance are to be prepared.)

    Module III (34 Hrs. - 3 Printouts, 4 Drawing sheets)

    a) Assembly Drawings: Engine parts and other machine parts stuffing boxes - cross heads Eccentrics - Petrol Engine connecting rod - Piston assembly - Screws jacks - Machine Vices Tailstock Crane hook.b) Assembly Drawings: Steam stop valve - Spring loaded safety valve Blow-off-cock -Gate valve-Glob valve-Ball valve- Non return valve(Scaled drawings of assembled viewsare tobe practiced).

    Note:

    Drawing practical classes have to be conducted by using any standard CAD software

    and using drawing instruments in alternative weeks (3 Hours) preferably for eachhalf of the students. Semester End examination (3 Hours) shall be conducted byusing drawing instruments only.

    All drawing exercises mentioned above are for class work. Additional exercises

    where ever necessary may be given as home assignments.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    16/249

    References Books:

    1. N.D. Bhatt and Panchal,Machine Drawing, Charator Publishing House.2. Gautam Pohit & Gautam Ghosh,Machine Drawing with AUTO CAD, Pearson Education,

    New Delhi.

    3. K.C. John, Machine Drawing, Jet Publications, Thrissur.4. N.D.Junnarkar,Machine Drawing, Pearson Education, New Delhi.5. P.I.Vargheese,Machine Drawing, VIP Publishers, Thrissur

    Internal AssessmentPrintouts (Best 5) 05x02 = 10Drawing sheets (Best 8) 08x01 = 08Tests (Best 2) 02x05 = 10Attendance and Regularity = 02Total = 30

    University examination patternQuestion I: Two questions of 15 marks each from (a) and (b) sections of module I.Question II: Two questions of 20 marks each from (a) and (b) sections of module II.Question III: Two questions of 35 marks each from (a) and (b) sections of module III.Total = 70 marks

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    17/249

    N09 305: Electrical Technology

    Teaching schemeCredits: 4

    3 hours lecture and 1 hour tutorial per week

    Objective

    To study the performance of different dc and ac machines

    To familiarise various electrical measuring instruments

    To give an overview of electric drives and power electronic control scheme

    Module I (12hours)Review of DC generators DC generator on no load open circuit characteristics basics ofarmature reaction and commutation load characteristics of shunt, series and compound

    generators Review of dc motors characteristics of shunt, series and compound motors starter 3 point and 4 point starters losses in DC machines power flow diagram efficiency applications of DC motors.

    Module II (12 hours)Review of transformers Real transformer winding resistance and leakage reactance equivalent circuit phasor diagram voltage regulation losses and efficiency open circuitand short circuit test Autotransformer saving of copper 3 phase transformer - -, Y-Y, - Y, Y - connections applications.Principle of indicating instruments moving coil, moving iron and dynamometer typeinstruments extension of range of ammeter and voltmeter using current transformer and

    voltage transformer principle and working of induction type energy meter

    Module III (15hours)Review of alternators distribution and chording factor EMF equation armature reaction

    phasor diagram voltage regulation predetermination of voltage regulation by EMFmethod (7 Hrs.)Review of 3-phase induction motor slip rotor frequency equivalent circuit phasordiagram torque equation torque-slip characteristics losses and efficiency power flow

    diagram no-load and blocked rotor tests starting of 3-phase induction motors direct-on-line, auto transformer, star-delta and rotor resistance starting..(8 Hrs.)

    Module IV (15 hours)Electrical Drives - Parts of electrical drives - Choice of electric drives - Status of DC and ACdrives - Dynamics of Electric drives - Fundamental torque equations Speed torqueconventions and multiquadrant operation - Components of load torque - Nature andclassification of load torque - Steady-state stability load equalisation. (7 Hrs.)

    Power semiconductor devices - Symbol and control characteristics of SCR comparison ofSCR, TRIAC, MOSFET and IGBT Basic concepts of Rectifier (AC-DC) , Inverter (DC-AC) and Choppers (DC-DC) (no derivations) - Chopper control of separately excited dc motor -Three phase Induction motor drives - Stator voltage control - Frequency control - Voltage andfrequency control (8 Hrs.)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    18/249

    Text Books

    1. Vincent Del Toro,Electrical Engineering Fundamentals, Prentice-Hall of India2. Hughes,Electrical technology, Tata Mc Graw Hill

    3 Dubey G.K.,Fundamentals a/Electrical Drives, Narosa

    Reference Books

    1. K. Sawhney, Electrical and Electronics measuring Instruments, Dhanpat Rai & Sons.

    2. P.S. Bhimbra, Electrical Machinery, Khanna Publishers3. K. Murukesh Kumar, DC machines and Transformers, Vikas Publishing house Pvt

    Ltd4. Rashid M.H, Power Electronics, Prentice Hall of India

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group discussions,

    quiz, literature survey, seminar, term-project, software exercises, etc.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    19/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2

    marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    20/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    21/249

    AN09 306: Metallurgy and Material Science

    Teaching scheme Credits: 43 hours lecture and I hour tutorial per week

    Objective: To impart knowledge on engineering materials, deformation of the crystals,

    equilibrium diagrams of selected alloy systems, heat treatment of steels, properties ofsteels, cast iron and other alloys, and its application

    Module I (10 hours)Introduction to materials science and engineering-Materials classification- Atomic structureand bonding -Primary Secondary bonding-Ionic, metallic, covalent, hydrogen-bonding-Crystallography -SC,FCC,BCC,HCP structures-APF-Miller indices-miller bravais indices-polymorphism- allotropy- density computations-Crystal structure determination-X-raydiffraction techniques- Microscopic examination- Specimen preparation-etching-

    Metallurgical microscope-SEM-TEM-Grain size determination

    Module II (15 hours)Imperfections in crystals- point defects, line defects, surface defects-Mechanical behavior ofmaterials- Elastic, visco elastic, anelastic behavior-Plastic Deformation of Metals and Alloys-Mechanisms of plastic deformation, role of Dislocation; slip and twinning- Schmids lawStrengthening mechanisms-grain size reduction-solid solution strengthening-Work hardening;recovery recrystallisation and grain growth Diffusion-laws of diffusion- Mechanisms of

    diffusion- applications-Fracture- ductile fracture, brittle fracture, fracture toughness, BT-Fatigue-s-n curve- creep- creep curve

    Module III (15 hours)Solidification of metals and alloys- Solid solution, Hume Rothery's rules-Phase diagrams-Phase and Lever Rules relationship of micro Structure and properties -Isomorphous systems-Cu-Ni -eutectic system- Pb-Sn- eutectoid - peritectic reactions- Iron- Carbon equilibriumdiagram. Development of microstructure in Iron Carbon alloys, Phase transformation in steel.

    TTT diagram, Heat treatment of steel, Annealing, tempering, austempering, martempering,Hardenability, Jomni test- surface hardening methods

    Module IV (14 hours)Applications of ferrous and non ferrous alloys-steel- low, medium, high carbon steels-Stainless steels-ferritic, austenitic, martensitic, duplex steels-tool steels cast iron- gray, white,ductile cast irons- copper and its alloys- aluminium and its alloys-magnesium and alloys-

    titanium and its alloys-refractories- super alloys-ceramics-PZT -PZLT-refractories-compositeand glasses-shape memory alloys- Nano materials-bio materials-Optical fibers

    Text Books1. William D Callister,Material science and engineering,2. Raghavan V,Material science and engineering,

    Reference Books1. Shackelford,Materials science for Engineers,2. Van Vlack,Materials science and Engineering,

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    22/249

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)

    30% - Assignments (minimum 2) such as home work, problem solving, group discussions,quiz, literature survey, seminar, term-project, software exercises, etc.

    10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    23/249

    University Examination Pattern

    PART A:Short

    answer

    questions

    (one/twosentence

    s)

    5 x 2marks=1

    0 marks

    All

    questionsarecompuls

    ory.

    Thereshould

    be atleast one

    question

    fromeach

    moduleand not

    more

    than twoquestions

    from anymodule.

    PART B:Analytic

    al/Problem

    solving

    questions

    4 x 5

    marks=20 marks

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    24/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    25/249

    AN09 307(P): Electrical Technology Lab

    Teaching Scheme Credits: 23 hours practical per week

    Objective

    To familiarize various electrical measurement equipments and measurement methods

    To obtain the performance characteristics of dc and ac machines

    1. Calibration of single phase energy meter ( Induction and Static type) by direct loading2. Load test on DC shunt generator

    a. Plot external characteristicsb. Deduce internal characteristics

    3. Load test on 3-phase squirrel cage induction motor.4. Load test on DC series motor

    a. Plot the performance characteristics5. Measurement of 3-phase power by using two-wattmeter method.6. Determination of V-I characteristics of linear resistance and incandescent lamp7. No-load and blocked rotor tests on slip ring induction motor

    a. Determine equivalent circuit parametersb. Predetermine the torque, line current and efficiency from equivalent circuit

    corresponding to a specified slip.

    8. Measurement of L,M & K of i) transformer windings and ii) air core coil.9. OC & SC tests on 3-phase alternator

    a. Predetermine the voltage regulation at various loads and different power

    factors by EMF method.10. Load test on single phase transformer

    a. Determine efficiency and regulation at various loads and unity power factor.11. OC & SC tests on single phase transformer

    a. Determine equivalent circuit parameters

    b. Predetermine efficiency and regulation at various loads and different powerfactors.

    12. Open circuit characteristics of dc shunt generatora. Plot OCC of rated speedb. Predetermine OCC for other speedsc. Determine critical field resistance for a specified speed

    d. Determine critical speed for a specified shunt field resistance

    Internal Continuous Assessment (Maximum Marks-50)

    60%-Laboratory practical and Record (30 marks)30%- Test/s (15 marks)10%- Regularity in the class (5 marks)

    Semester End Examination (Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)20% - Viva voce (10 marks)

    10% - Fair record (5 marks)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    26/249

    AN 09 308(P) PRODUCTION ENGINEERING LAB

    Teaching Scheme Credits: 23 hours practical per week

    Objective

    To acquaint the basics of lathe and accessories. ,shaping and slottng machine,

    planning machines

    To learn about different tools used for different operations.

    To impart training on plane turning, groove cutting, form turning, taper turning,

    facing and thread cutting.

    To impart exercise involving production of flat surfaces, grooves and keyways.

    Internal Continuous Assessment(Maximum Marks-50)

    60% - Workshop practicals and Record (30 marks)30% - Test/s (15 marks)

    10% - Regularity in the class (5 marks)

    Semester End Examination(Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)20% - Viva voce (10 marks)10% - Fair record (5 marks)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    27/249

    FOURTH SEMESTEREN09 401A: Engineering Mathematics IV

    (Common for ME, CE, PE, CH, BT, PT, AM, and AN)

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    ObjectiveThe use of probability models and statistical methods for analyzing data has become

    common practice in virtually all scientific disciplines. Two modules of this course attempt to provide a comprehensive introduction to those models and methods most likely to beencountered and used by students in their careers in engineering. A broad introduction tosome important partial differential equations is also included to make the student get

    acquainted with the basics of PDE.

    Module I: Probability Distributions (13 hours)Random variables Mean and Variance of probability distributions Binomial Distribution Poisson Distribution Poisson approximation to Binomial distribution Hyper GeometricDistribution Geometric Distribution Probability densities Normal Distribution Uniform Distribution Gamma Distribution.

    Module II: Theory of Inference (14 hours)Population and Samples Sampling Distribution Sampling distribution of Mean ( known)

    Sampling distribution of Mean ( unknown) Sampling distribution of Variance IntervalEstimation Confidence interval for Mean Null Hypothesis and Tests of Hypotheses Hypotheses concerning one mean Hypotheses concerning two means Estimation ofVariances Hypotheses concerning one variance Hypotheses concerning two variances Test of Goodness of fit.

    Module III: Series Solutions of Differential Equations (14 hours)Power series method for solving ordinary differential equations Legendres equation

    Legendre polynomials Rodrigues formula Generating functions Relation betweenLegendre polynomials Orthogonality property of Legendre polynomials (Proof notrequired) Frobenius method for solving ordinary differential equations Bessels equation Bessel functions Generating functions Relation between Bessel functions Orthogonalityproperty of Bessel functions (Proof not required).

    Module IV: Partial Differential Equations (13 hours)Introduction Formation of PDE Complete Solution Equations solvable by directintegration Linear PDE of First order, Legranges Equation: Pp + Qq = R Non-LinearPDE of First Order, F(p,q) =0 , Clairauts Form: z = px + qv + F(p,q) , F(z,p,q) =0 , F1(x,q) =F2(y,q) Classification of Linear PDEs Derivation of one dimensional wave equation andone dimensional heat equation Solution of these equation by the method of separation ofvariables DAlemberts solution of one dimensional wave equation.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    28/249

    Text Books

    Module I:Richard A Johnson, CB Gupta, Miller and Freunds Probability and statistics for Engineers,7e, Pearson Education- Sections: 4.1, 4.2, 4.3, 4.4, 4.6, 4.8, 5.1, 5.2, 5.5, 5.7

    Module II:Richard A Johnson, CB Gupta, Miller and Freunds Probability and statistics for Engineers,7e, Pearson Education- Sections: 6.1, 6.2, 6.3, 6.4, 7.2, 7.4, 7.5, 7.8, 8.1, 8.2, 8.3, 9.5

    Module III:Erwin Kreysig,Advanced Engineering Mathematics, 8e, John Wiley and Sons, Inc.-Sections: 4.1, 4.3, 4.4, 4.5

    Module IV:N Bali, M Goyal, C Watkins,Advanced Engineering Mathematics, A Computer Approach, 7e,

    Infinity Science Press, Fire Wall Media- Sections: 16.1, 16.2, 16.3, 16.4, 16.5, 16.6, 16.7,

    16.8, 16.9Erwin Kreysig,Advanced Engineering Mathematics, 8e, John Wiley and Sons, Inc.Sections: 11.2, 11.3, 11.4, 9.8 Ex.3, 11.5

    Reference books18 William Hines, Douglas Montgomery, avid Goldman, Connie Borror,Probability andStatistics in Engineering, 4e, John Wiley and Sons, Inc.19 Sheldon M Ross, Introduction to Probability and Statistics for Engineers andScientists, 3e, Elsevier, Academic Press.

    20 Anthony Croft, Robert Davison, Martin Hargreaves, Engineering Mathematics, 3e,

    Pearson Education.21 Parthasarathy,Engineering Mathematics, A Project & Problem based approach, AneBooks India.22 B. V Ramana,Higher Engineering Mathematics, McGrawHill.23 Sarveswara Rao Koneru,Engineering Mathematics, Universities Press.24 J K Sharma, Business Mathematics, Theory and Applications, Ane Books India.25 John bird,Higher Engineering Mathematics, Elsevier, Newnes.26 M Chandra Mohan, Vargheese Philip,Engineering Mathematics-Vol. I, II, III & IV.,Sanguine Technical Publishers.

    27 Wylie C.R and L.C. Barret,Advanced Engineering Mathematics, McGraw Hill.28 V R Lakshmy Gorty,Advanced Engineering Mathematics-Vol. I, II., Ane Books India.29 Sastry S.S.,Advanced Engineering Mathematics-Vol. I and II., Prentice Hall of India.

    30 Michael D Greenberg,Advanced Engineering Mathematics, Pearson Education.

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group discussions,

    quiz, literature survey, seminar, term-project, software exercises, etc.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    29/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    30/249

    University Examination Pattern

    PART A:Short

    answerquestions(one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    arecompulsory. Thereshould be

    at leastonequestionfrom eachmoduleand notmore thantwo

    questionsfrom any

    module.

    PART B:

    Analytical/Problemsolvingquestions4 x 5marks=20 marks

    Candidates have toanswerfour

    questionsout of six.Thereshould be

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    31/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    32/249

    EN09 402: Environmental Science(Common for all branches)

    Teaching scheme Credits: 32 hours lecture and 1 hour tutorial per week

    Objective To understand the problems of pollution,loss of forest,solid waste

    disposal,degradation of environment,loss of biodiversity and other environmentalissues and create awareness among the students to address these issues andconserve the environment in a better way.

    Module I (8 hours)The Multidisciplinary nature of environmental scienceDefinition-scope and importance-need for public awareness.Natural resources

    Renewable and non-renewable resources:Natural resources and associated problems-forest resources: Use and over exploitation,deforestation, case studies. Timber extraction, mining, dams and their defects on forests andtribal people.- water resources: Use and over utilization of surface and ground water,

    floods ,drought ,conflicts over water, dams-benefits and problems.- Mineral resources: Useand exploitation,environmental effects of extracting and using mineral resources, casestudies.- Food resources: World food problems, changes caused by agriculture over grazing,effects of modern agriculture, fertilizer-pesticide problems, water logging,salinity,casestudies.-Energy resources: Growing energy needs, renewable and non-renewable energyresources, use of alternate energy resources,Land resources: Land as a resource, landdegradation, man induced land slides, soil erosion and desertification.

    Module II (8 hours)Ecosystems-Concept of an ecosystem-structure and function of an ecosystem producers,

    consumers, decomposers-energy flow in the ecosystem-Ecological succession- Food chains,food webs and Ecological pyramids-Introduction, types, characteristics features, structure andfunction of the following ecosystem-Forest ecosystem- Grassland ecosystem Desertecosystem-Aquatic ecosystem(ponds, streams, lakes, rivers, oceans , estuaries)Biodiversity and its considerationIntroduction- Definition: genetic , species and ecosystem diversity-Biogeographical;classification of India value of biodiversity: consumptive use, productive use, social ethical ,aesthetic and option values Biodiversity at Global, national , and local level-India at mega

    diversity nation- Hot spot of biodiversity-Threats to biodiversity: habitat loss, poaching of

    wild life, man , wild life conflicts Endangered and endemic species of India-Conservation ofbiodiversity : In-situ and Ex-situ conservation of biodiversity.

    Module III (10 hours)Environmental pollutionDefinition-Causes, effects and control measures of Air pollution-m Water pollution soilpollution-Marine pollution-Noise pollution-Thermal pollution-Nuclear hazards-Solid waste

    management: Causes, effects and control measures of urban and industrial wastes-Role of anindividual in prevention of pollution-pollution case studies-Disaster management: floods ,earth quake, cyclone and landslides-Environmental impact assessment

    Module IV (10 hours)

    Environment and sustainable development-Sustainable use of natural resources-Conversionof renewable energy resources into other forms-case studies-Problems related to energy and

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    33/249

    Energy auditing-Water conservation,rain water harvesting,water shed management-casestudies-Climate change,global warming,acid rain,ozone layer depletion,nuclear accidentsandholocaust-Waste land reclamation-Consumerism and waste products-Reduce,reuse andrecycling of products-Value education.

    Text Books1. Clark,R.S.Marine pollution,Clanderson Press Oxford.2. Mhaskar A. K. Matter Hazrdous, Techno-science Publications.

    3. Miller T. G. Jr., Environmental Science, Wadsworth Publishing Co.4. Townsend C., Harper J, Michael Begon, Essential of Ecology, Blackwell Science

    5. Trivedi R. K., Goel P. K., Introduction to Air Pollution, Techno-Science Publications.

    Reference Books.

    1. Raghavan Nambiar,K Text book of Environmental Studies,Nalpat Publishers, Kochi

    2. 3. Bharucha Erach, Biodiversity of India, Mapin Publishing Pvt. Ltd., Ahmedabad 380

    013, India, Email: [email protected]. Cunningham, W.P., Cooper, T.H., Gorhani, E & Hepworth, M.T. 2001Environmental

    encyclopedia Jaico publ. House Mumbai 1196p5. Down to Earth, Centre for Science and Environment

    6. Hawkins, R.E. Encyclopedia of Indian Natural History, Bombay Natural HistorySociety, Bombay

    7. Mckinney, M.L. & School, R.M. 1996. Environmental Science system & Solutions,Web enhanced edition, 639p.

    8. Odum, E.P. 1971. Fundamentals of Ecology. W.B.Saunders Co. USA, 574p

    9. Rao, M.N. & Datta, A.K 1987. Waste Water treatment. Oxford & IBH Publ. Co. Pvt.Ltd., 345p10. Survey of the Environment, The Hindu (M)11. Wagner.K.D. 1998. Environmental Management. W.B. Saunders Co. Philadelphia,

    USA 499p

    12. *M Magazine

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as Report of field work, literature survey, seminar

    etc.

    10% - Regularity in the class

    Note: Field work can be Visit to a local area to document environmental assets-river/forest/grass land/mountain or Visit to local polluted site-

    urban/rural/industrial/agricultural etc. or Study of common plants,insects,birdsetc.or Study of simple ecosystems-pond,river,hill slopes etc.or mini project workon renewable energy and other naturaral resources , management of wastes etc.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    34/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    35/249

    University Examination Pattern

    PART A:Short

    answerquestions

    (one/twosentences

    )5 x 2

    marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5

    marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    36/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    37/249

    AN09 403 AIRCRAFT STRUCTURES-I

    Teaching scheme credits54 hours lecture and I hour tutorial per week

    OBJECTIVE

    To study different types of beams and columns subjected to various types of loading

    and support conditions with particular emphasis on aircraft structural components.

    MODULE 1 (20 hours)

    Statically determinate structures

    Analysis of plane truss -Method of joints -3 D Truss -Plane frames

    Statically indeterminate structures

    Composite beam -Clapeyron's Three Moment Equation -Moment Distribution Method.

    MODULE 2(17hours)EnergyStrain Energy due to axial, bending and Torsional loads -Castigliano's theorem -Maxwell'sReciprocal theorem, Unit load method -application to beams, trusses, frames, rings, etc.

    MODULE 3 (19hours)

    ColumnsColumns with various end conditions -Euler's Column curve -Rankine's formula

    Column with initial curvature -Eccentric loading -South well plot -Beam column.

    MODULE 4 (16 hours)

    Failure theory

    Maximum Stress theory -Maximum Strain Theory -Maximum Shear Stress Theory

    -Distortion Theory Maximum Strain energy theory -Application to aircraft Structural

    problems.

    TEXT BOOK

    Donaldson, B.K., "Analysis of Aircraft Structures -An Introduction", McGraw-Hill, 1993.

    REFERENCETimoshenko, S., "Strength of Materials", Vol. I and II, Princeton D. Von Nostrand Co, 1990.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    38/249

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)

    30% - Assignments (minimum 2) such as home work, problem solving, groupdiscussions, quiz, literature survey, seminar, term-project, software exercises,etc.

    10% - Regularity in the class

    University Examination Pattern

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    39/249

    PART A:Short

    answer

    questions

    (one/twosentence

    s)

    5 x 2marks=1

    0 marks

    Allquestions

    are

    compulsory.

    Thereshould

    be at

    least onequestion

    fromeach

    module

    and notmore

    than twoquestions

    from any

    module.

    PART B:Analytic

    al/Proble

    msolving

    questions

    4 x 5

    marks=20 marks

    Candidat

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    40/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    41/249

    AN09 404 HEAT TRANSFER

    Teaching scheme Credits: 43 hours lecture and I hour tutorial per week

    ObjectiveTo introduce the concepts of heat transfer to enable the students to design components

    subjected to thermal loading.

    Module 1.(10hours)Heat conductionBasic Modes of Heat Transfer -One dimensional steady state heat conduction: CompositeMedium Critical thickness -Effect of variation of thermal Conductivity -Extended Surfaces

    -Unsteady state. Heat Conduction: Lumped System Analysis -Heat Transfer in Semi infiniteand infinite solids -Use of Transient -Temperature charts -Application of numericaltechniques.

    Module 2. (10hours)Convective heat transferIntroduction -Free convection in atmosphere free convection on a vertical flat plate-Empirical relation in free convection -Forced convection -Laminar and turbulent convectiveheat transfer analysis in flows between parallel plates, over a flat plate and in a circular pipe.Empirical relations, application of numerical techniques in problem solving.

    Module 3. (20hours)Radiative heat transferIntroduction to Physical mechanism -Radiation properties -Radiation shape factors -Heatexchange between non -black bodies -Radiation shields.Heat exchangersClassification -Temperature Distribution -Overall heat transfer coefficient, Heat ExchangeAnalysis LMTD Method and E-NTU Method.

    Module 4(14 hours)Heat transfer problemsHeat transfer problems in aerospace engineering High-Speed flow Heat Transfer, HeatTransfer problems in gas turbine combustion chambers -Rocket thrust chambers

    -Aerodynamic heating -Ablative heat transfer.

    Text books

    1. J. Yunus A. Cengel., "Heat Transfer -A practical approach", Second Edition, Tata

    McGraw-Hill, 2002.

    2. Incropera. F.P .and Dewitt.D.P. Introduction to Heat Transfer", John Wiley and Sons

    -2002.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    42/249

    References

    1.Lienhard, J.H., "A Heat Transfer Text Book", Prentice Hall Jnc. 1981.

    2.Holman, J.P. "Heat Transfer", McGraw-Hill Book Co., Inc., New York, 6th Edn. 1991.

    3.Sachdeva S C, "Fundamentals of Engineering Heat & Mass Transfer", Wiley Eastern Ltd.,New Delhi, 1981.

    4.Mathur M. and Sharma, R.P. "Gas Turbine and Jet and Rocket Propulsion", Standard

    Publishers, New Delhi 1988.

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, group

    discussions, quiz, literature survey, seminar, term-project, software exercises,etc.

    10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    43/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    44/249

    AN09 405: Mechanics of SolidsTeaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    Objective

    To acquaint with the basic concepts of stress and deformation in solids.

    To practise the methodologies to analyse stresses and strains in simple

    structural members, and to apply the results in simple design problems.

    Module I (14 hours)Simple Stress and Strain: Introduction to analysis of deformable bodies internal forces method of sections assumptions and limitations. Simple stresses stresses due to normal,

    shear and bearing loads strength design of simple members. Axial and shear strains Material behaviour uniaxial tension test stress-strain diagrams concepts of orthotropy,anisotropy and inelastic behaviour Hookes law for linearly elastic isotropic material underaxial and shear deformation deformation in axially loaded bars thermal effects staticallyindeterminate problems principle of superposition. Elastic strain energy for uniaxial stress.Definition of stress and strain at a point (introduction to stress and strain tensors and itscomponents only) Poissons ratio biaxial and triaxial deformations Bulk modulus -Relations between elastic constants.

    Module II (14 hours)Torsion: Torsion theory of elastic circular bars assumptions and limitations polar modulus- torsional rigidity economic cross-sections statically indeterminate problems design for

    torsional load (shaft and flanged bolt coupling) torsion of inelastic circular bars(introduction only).Axial force, shear force and bending moment: Diagrammatic conventions for supports andloading - axial force, shear force and bending moment in a beam differential relations

    between load, shear force and bending moment - shear force and bending moment diagramsby direct and summation approach - use of singularity functions elastic curve point ofinflection.

    Module III (13 hours)Stresses in beams: Pure bending flexure formula for beams assumptions and limitations section modulus - flexural rigidity - economic sections beam of uniform strength.Shearing stress formula for beams assumptions and limitations - shear flow design for

    flexure and shear (reinforced beams, fliched beams, etc.) inelastic bending (introductiononly).

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    45/249

    Deflection of beams: Moment-curvature relation assumptions and limitations - doubleintegration method - singularity functions Macaulays method superposition techniques moment area method and conjugate beam ideas for simple cases elementary treatment ofstatically indeterminate beams.

    Module IV (13 hours)Transformation of stress and strains: Plane state of stress - equations of transformation -principal stresses. Plane state of strain analogy between stress and strain transformation -

    Mohrs circles of stress and strain strain rosettes.Compound stresses: Combined axial, flexural and shear loads eccentric loading undertension/compression - kern of a section (rectangular and circular section) - combined bendingand twisting loads.Theory of columns: Buckling theory Eulers formula for long columns assumptions andlimitations Text effect of end conditions - slenderness ratio Rankines formula forintermediate columns Eccentric loading of columns secant formula.

    Text Books

    13. E. P. Popov, T. A. Balan, Engineering Mechanics of Solids, Pearson Education, New

    Delhi.14. A. Pytel, F. L. Singer, Strength of Materials, Harper & Row Publishers, New York.

    15. P. N. Singh, P. K. Jha, Elementary Mechanics of Solids, Wiley Eastern Limited, NewDelhi.

    Reference Books

    1. Gere, Timoshenko, ,Mechanics of Materials, CBS Publishers & Distributors, New Delhi.2. I. H. Shames, J. H. Pitarresi,Introduction to Solid Mechanics, Prentice Hall of India, New

    Delhi.3. F. Beer, E. R. Johnston, J. T. DeWolf, Mechanics of Materials, Tata McGraw Hill, New

    Delhi

    4. S. H. Crandal, N. C. Dhal, T. J. Lardner, An Introduction to the Mechanics of

    Solids, McGraw Hill

    Internal Continuous Assessment (Maximum Marks-30)

    60% - Tests (minimum 2)

    30% - Assignments (minimum 2) such as home work, problem solving, etc.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    46/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    47/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    48/249

    AN09 406 ELEMENTS OF AERONAUTICS

    Teaching scheme Credits: 43 hours lecture and I hour tutorial per week

    ObjectiveTo introduce the basic concepts of aerospace engineering and the current

    developments in the field.

    Module 1

    Historical evaluation (14hours)

    Early airplanes, biplanes and monoplanes, Developments in aerodynamics, materials,structures and propulsion over the years.

    Aircraft configurations

    Components of an airplane and their functions. Different types of flight vehicles,classifications. Conventional control, Powered control, Basic instruments for flying, Typicalsystems for control actuation.

    Module 2(12 hours)

    Introduction to principles of flight

    Physical properties and structure of the atmosphere, Temperature, pressure and altitude

    relationships, Evolution of lift, drag and moment. Aerofoils, Mach number, Maneuvers.

    Module 3(13hours)

    Introduction to airplane structures and materials (14hours)

    General types of construction, Monocoque, semi-monocoque and geodesic construction,

    Typical wing and fuselage structure. Metallic and non-metallic materials, Use of aluminum

    alloy, titanium, stainless steel and composite materials.

    Module 4 (13hours)

    Power plants used in airplanesBasic ideas about piston, turboprop and jet engines, Use of propeller and jets for thrust

    production. Comparative merits, Principles of operation of rocket, types of rockets and typical

    applications, Exploration into space.

    Text book

    I. Anderson, J.D., "Introduction to Flight", McGraw-Hi II, 1995.

    Reference

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    49/249

    Kermode, A.c., "Flight without Formulae", McGraw Hill, 1997

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    50/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolvingquestions4 x 5marks=20 marks

    Candidates have toanswerfourquestionsout of six.There

    should beat least

    onequestionfrom eachmodule

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    51/249

    AN09 407(P): Material Testing Lab

    Teaching scheme Credits: 23 hours practical per week

    Objective

    To provide knowledge on the mechanical behaviour of materials.

    To acquaint with the experimental methods to determine the mechanical

    properties of materials.

    1. Standard tension test on mild steel using Universal Testing Machines and suitableextensometers

    2. Stress-strain characteristics of brittle materials cast iron

    3. Spring test open and closed coiled springs determination of spring stiffness andmodulus of rigidity

    4. Determination of modulus of rigidity of wires5. Hardness tests Brinnell hardness, Rockwell hardness (B S C scales), Rockwell

    superficial hardness (N & T scales), and Vickers hardness

    6. Impact test Izod and Charpy7. Bending test on wooden beams

    8. Fatigue testing study of testing machine9. Photoelastic method of stress measurements (two dimensional problems)10. Torsion test on mild steel rod11. Shear test on mild steel rod

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    52/249

    Reference Books

    1. G. E. Dieter, Mechanical Metallurgy, McGraw Hill.J. W. Dally, W. P. Railey,Experimental Stress Analysis, McGraw Hill

    Internal Continuous Assessment(Maximum Marks-50)

    60% - Practicals and record (30 marks)30% - Test/s (15 marks)10% - Regularity in the class (5 marks)

    Semester End Examination(Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)20% - Viva voce (10 marks)

    10% - Fair record (5 marks)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    53/249

    AN09 408(P) AIRCRAFT STRUCTURES LAB-I

    Teaching scheme Credits: 23 hours practical per week

    Objective

    To study experimentally the load deflection characteristics structural materials under

    different types of loads.

    List of experiments

    1. Determination of Young's modulus of steel using mechanical extensometers.

    2. Determination of Young's modulus of aluminum using electrical extensometers

    3. Determination of fracture strength and fracture pattern of ductile materials

    4. Determination of fracture strength and fracture pattern of brittle materials

    5. Stress Strain curve for various engineering materials.

    6. Deflection of beams with various end conditions.

    7. Verification of Maxwell's Reciprocal theorem & principle of superposition

    8. Column -Testing

    9. South -well's plot.

    10. Riveted Joints.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    54/249

    LIST OF EQUIPMENTS

    (For batch of30 students)

    SI. No. Equipments Qty Experiments

    No.

    1. Universal Testing Machine 1 1,2,3,4,5,10

    2. Mechanical Extensometer 1 1

    3. Electrical stain gauge 10 2

    4. Stain indicator 1 2

    5. Dial Gauges 12 3,4

    6. Beam Test set up with various end conditions 2 3,4

    7. Weight I Kg 10 3,4

    8. Weight 2 Kg 10 3,4

    9. Weight Pans 6 3,4

    10. Column Test Apparatus 1 5,6

    11. Rivet 30 10

    Internal Continuous Assessment(Maximum Marks-50)

    60% - Practicals and record (30 marks)30% - Test/s (15 marks)

    10% - Regularity in the class (5 marks)

    Semester End Examination(Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)20% - Viva voce (10 marks)

    10% - Fair record (5 marks)

    SEMESTER V

    AN09 501 MICROPROCESSORS AND APPLICATIONS

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    55/249

    Teaching scheme Credits: 54 hours lecture and 1 hour tutorial per week

    Objective

    To give the principle and applications of microprocessors to the students

    Module 1. (18 hours)Semiconductor devicesPN Junction diodes -Zenor Diodes -Tunnels Diodes-Thermistors -Transistors -FET and

    MOSFET Silicon Controlled Rectifiers And Triacs -Their Applications -Half Wave and FullWave Rectifiers Filters -Ripple Factor -Zenor Regulators and AC Voltage Regulators-Principles and Types of Transistor Amplifiers -RC Coupled, Transformer Coupled, DirectCoupled -Multistage, F:T and Power Amplifers.

    Module 2.(18 hours)Linear and digital icsIC Technology -Elements of Fabrication of Linear and Digital IC's -DIA and AID ConvertersComparison Between Analog and Digital Systems -Number Representation -Binary, Octaland Hexadecimal Number Systems -Logic Families and Logic Gates -Flip -Flops -MultiVibrations Using IC's -Half and full Adder -Registers -Counters -Multiplexers-Demultiplexers-Decoders -Encoders.

    Module 3. (18 hours)Microprocessors

    Block Diagram of Microprocessors -Architecture of Intel 8085 -Importance of Data, Addressand Control Buses -Instruction Formats -Addressing Modes and Types of Intel 8085-Instruction Set For 8085 Development of Simple Language Assembly Programs-Architecture and Functioning of Processors like Z80, M6800 and Intel Family of 80 X86Processors.

    Module 4.(18 hours)Microprocessor memory devices (18hours)RAM, ROM, EPROM -magnetic Bubble Memory -Floppy and Hard Disc -Interfacing ofMemory Chips -CRT Terminals -Printers, Keyboards and their Interfacing -Parallel and SeriesCommunication Synchronous and Asynchronous Data Transfer -DMA Data Transfer.APPLICATIONS: Microprocessor Applications in aerospace -Case study.

    TEXTBOOKS

    I. "Computer principles of architecture", Tata McGraw-Hill, New Delhi. 4 th Edition 2002.

    1.Goankar. R.S., "Microprocessors, Programming to Architecture 8085", Penram Internationalpublishing PVT Ltd, New Delhi. 5th Edition 2002

    V.K. Mehta, "Principles of Electronics", S. Chand & Co, New Delhi, 2nd Edition 2002

    References

    1. Goankar R.S., "Microprocessors Architecture. Programming and Applications", WileyEastern, 1992.

    2. Ajit Pal., "Microprocessors", Tata McGraw-Hill, Revised Edition 1995.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    56/249

    3. Douglas, Hall, "Microprocessors and Interfacing", Tata McGraw-Hill, RevisedEdition 1990.

    4. Mathur A.P., "Introduction to Microprocessors", Tata McGraw-Hill, Revised Edition1995.

    5. Malvino A.P. Leach, D.P., "Digital Principles & Applications", Tata McGraw-Hill,1990.

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc. Atleast one

    assignment should be programming / problem solving using computers.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    57/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    58/249

    AN09 502 CONTROL ENGINEERING

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    Objective

    To understand the basic concepts of flight control systems.

    Module 1.(14 hours)

    Introduction

    Historical review -Simple pneumatic, hydraulic and thermal systems, Series and parallelsystems, Analogies -Mechanical and electrical components, Development of flight controlsystems.

    Open and closed loop systems

    Feedback control systems -Block diagram representation of control systems, Reduction ofblock diagrams, Output to input ratios, Signal flow graph.

    Module 2.(12hours)

    Characteristic Equation and Functions

    Lap lace transformation, Response of systems to different inputs viz., Step input, impulse,ramp, parabolic and sinusoidal inputs, Time response of first and second order systems,steady state errors and error constants of unity feedback circuit.

    Module 3. (15hours)

    Concept of stability

    Necessary and sufficient conditions, Routh -Hurwitz criteria of stability, Root locus and Bodetechniques, Concept and construction, frequency response.

    Module 4. (13hours)

    SAMPLED DATA SYSTEMS: Introduction to digital control system, Digital

    Controllers and Digital PID Controllers.

    Text booksI. OGATO, "Modern Control Engineering", Prentice -Hall of India Pvt. Ltd. New Delhi, 1998.

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    59/249

    2. GOPAL.M. "Control Systems, Principles and design" -Tata McGraw-Hill Publication, NewDelhi, 2000.

    REFERENCES

    I. Azzo, .J.D. and C.H. Houpis, "Feed back control system analysis and synthesis", McGraw-Hill International, 3rd Edition, 1998.

    1.Kuo, B.C., "Automatic control systems", Prentice -Hall of India Pvt. Ltd., New Delhi, 1998.3. Houpis, C.H. and Lamont, G.B., "Digital Control Systems", McGraw-Hili Book Co. NewYork, USA 1995.4. Naresh K. Sinha, "Control Systems", New Age International Publishers, New Delhi

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc. Atleast one

    assignment should be programming / problem solving using computers.10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    60/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    61/249

    AN09 503 NUMERICAL METHODS

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    Objective

    With the present development of computer technology, it is necessary to develop efficient

    algorithms for solving problems in science, engineering and technology. This course gives a

    complete procedure for solving different kinds of problems occur in engineering numerically.

    At the end of the course, the students would be acquainted with the basic concepts in

    numerical methods and their uses.

    Module 1.(14hours)

    Solution of equations and eigen value problems

    Linear Interpolation Methods (Method of False Position) -Newton's Method -Statement of

    Fixed Point Theorem -Fixed Pointer Iteration X=G(X) Method -Solution of Linear System of

    Gaussian Elimination and Gauss-Jordan Methods -Iterative Methods: Gauss Jacobi and Gauss

    -Seidel Methods-Inverse of A Matrix by Gauss-Jordan Method. Eigen Value of a Matrix by

    Power Methods.

    Module 2.(14hours)

    Interpolation and approximation

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    62/249

    Lagrangian Polynomials -Divided difference -Interpolation with a cubic spline -Newton

    forward and backward difference formulae.

    Module 3. (14hours)

    Numerical differentiation and integration

    Derivatives from difference table -Divided difference and finite difference -Numerical

    integration by Trapezoidal and Simpson's 1/3 and 3/8 rules -Romberg's method -Two and

    three point Gaussian quadrature formulas -Double integrals using trapezoidal and Simpson's

    rules..

    Module 4.(14 hours)

    Initial value problems for ordinary differential

    Equations

    single step methods : Taylor series and methods -Euler and modified Euler methods -fourth

    order Runge-Kutta method for solving first and second order equations -multistep methods

    -Milnes and Adams predictor and corrector methods. Boundary value problems. Finite

    difference solution for the second order ordinary differential equations. Finite difference

    solution for one dimensional heat equation by implicit and explicit methods -one dimensional

    wave equation and two dimensional Laplace and Poisson equations.

    Text booksI. Gerald, C.F, and Wheatley, P.O, "Applied Numerical Analysis", Sixth Edition, PearsonEducation Asia, New Delhi, 2002.2. Balagurusamy, E., "Numerical Methods", Tata McGraw-Hili Pub. Co. Ltd., New Delhi,1999.

    References

    1. Kandasamy, P.Thilakavthy, K and Gunavathy, K.Numerical Methods. S.Chand and Co.

    New Delhi,1999

    2. Burden, R.L and Faries, T.D., "Numerical Analysis", Seventh Edition, Thomson Asia Pvt.

    Ltd., Singapore, 2002.

    3. Venkatraman M.K, "Numerical Methods" National Pub. Company, Chennai, 1991.

    Sankara Rao K., "Numerical Methods for Scientists and Engineers", 2 nd Ed. Prentice Hall,India,2004

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc. Atleast one

    assignment should be programming / problem solving using computers.

    10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    63/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    64/249

    AN09 504 FLIGHT DYNAMICS

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    OBJECTIVE

    To study the performance of airplanes under various operating conditions and thestatic and dynamic response of aircraft for both voluntary and involuntary changes inflight conditions

    Module 1.(15hours)Drag on the airplaneInternational Standard Atmosphere - Forces and moments acting on a flight vehicle - Equationof motion of a rigid flight vehicle - Different types of drag - Drag polars of vehicles from low

    speed to high speeds - Variation of thrust, power and SFC with velocity and altitudes for airbreathing engines and rockets - Power available and power required curves.

    Aircraft performancePerformance of airplane in level flight - Maximum speed in level flight - Conditions forminimum drag and power required - Range and endurance - Climbing and gliding flight(Maximum rate of climb and steepest angle of climb, minimum rate of sink and shallowestangle of glide) -Turning performance (Turning rate turn radius). Bank angle and load factor -

    Limitations of pull up and push up digram and load factor

    Module 2.(12hours)Static longitudinal stabilityDegree of freedom of rigid bodies in space - Static and dynamic stability - Purpose of controlsin airplanes - Inherently stable and marginal stable airplanes - Static, Longitudinal stability -Stick fixed stability - Basic equilibrium equation - Stability criterion - Effects of fuselage andnacelle - Influence of CG location Power effects - Stick fixed neutral point - Stick freestability-Hinge moment coefficient - Stick free neutral points-Symmetric maneuvers - Stickforce gradients Stick force per 'g' - Aerodynamic balancing-Determination of neutral points

    and maneuver points from flight test.

    Module 3(13 hours)Lateral and directional stabilityDihedral effect- Lateral control-coupling between rolling and yawing moments-Adverse yaw

    effects- Aileron reversal-Statc directional stability-Weather cocking effect-Rudderrequirements-one engine inoperative condition-Rudder lock

    Module 4 (14 hours)Dynamic stabilityDynamic Longitudinal stability Equationd of motion Stability derivatives characteristicsequation of stick fixed case Modes and stability criterion Effect of freezing the stick Briefdescription of lateral and directional. Dynamic stability Spiral,Divergence,Dutch roll,autorotaton and spin

    Text Book

    1. Perkins C.D and Hage.R.E. Airplane performance stability and control,John Wiley &son 1988

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    65/249

    References1. Etkin B Dynamics of flight stability and control John wiley 1982

    2. Babister A.W Air craft dynamic stability and response, Pergamamon pressOxford 1980

    3. Dommasch.D.O, Shelby, and Connolly.T.F Aeroplane Aero dynamics Thirdedition Issac Pitman, London 19814. Nelson.R.C.Flight stability and Automatic Control McGraw-Hill Book Co

    1998

    Internal Continuous Assessment(Maximum Marks-30)

    60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc. Atleast one

    assignment should be programming / problem solving using computers.

    10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    66/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    67/249

    AN09 505 AIRCRAFT STRUCTURES -II

    Teaching scheme Credits: 43 hours lecture and 1 hour tutorial per week

    Objective

    To study the behavior of various aircraft structural components under different types of loads.

    Module 1(11 hours)

    Unsymmetrical bendingBending stresses in beams of unsymmetrical sections -Bending of symmetric sections with

    skew loads.

    Module 2(11hours)Shear flow in open sectionsThin walled beams, Concept of shear flow, shear centre, Elastic axis. With one axis ofsymmetry, with wall effective and ineffective in bending, unsymmetrical beam sections.

    Module 3.(11 hours)Shear flow in closed sectionsBredt -Batho formula, Single and multi -cell structures. Approximate methods. Shear flow in

    single & multicell structures under torsion. Shear flow in single and multicell under bendingwith walls effective and ineffective.

    Module4. (20hours)Buckling of platesRectangular sheets under compression, Local buckling stress of thin walled sections,

    Crippling stresses by Needham's and Gerard's methods, Thin walled column strength. Sheetstiffener panels. Effective width, inter rivet and sheet wrinkling failures.

    Stress analysis in wing and fuselageProcedure -Shear and bending moment distribution for semi cantilever and other types ofwings and fuselage, thin webbed beam. With parallel and non parallel flanges, Shear resistantweb beams, Tension field web beams (Wagner's).

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    68/249

    Text book

    Peery, D.1., and Azar, J.J., "Aircraft Structures", 2nd edition, McGraw-Hill, N.Y., 1993.

    References

    I. Megson, T.M.G., "Aircraft Structures for Engineering Students", Edward Arnold, 1995.1.Bruhn. E.H. "Analysis and Design of Flight vehicles Structures", Tri -state off set company,USA, 1985.

    Rivello, R.M., "Theory and Analysis of Flight Structures", McGraw-Hill, 1993

    Internal Continuous Assessment(Maximum Marks-30)60% - Tests (minimum 2)30% - Assignments (minimum 2) such as home work, problem solving, etc. Atleast one

    assignment should be programming / problem solving using computers.

    10% - Regularity in the class

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    69/249

    University Examination Pattern

    PART A:Shortanswerquestions

    (one/twosentences

    )5 x 2marks=10 marks

    Allquestions

    are

    compulsory. Thereshould beat leastonequestionfrom each

    moduleand notmore thantwoquestions

    from anymodule.

    PART B:Analytical/Problemsolving

    questions4 x 5marks=20 marks

    Candidates have toanswer

    fourquestions

    out of six.Thereshould beat least

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    70/249

    AN09 506 AERODYNAMICS -I

    Teaching scheme Credits: 32 hours lecture and 1 hour tutorial per week

    Objective

    To understand the behaviour of airflow over bodies with particular emphasis on airfoilsections in the incompressible flow regime.

    Module 1. (4hours)

    REVIEW OF BASIC FLUID MECHANICS

    Continuity, momentum and energy equations.

    Module 2. (10hours)

    Two dimensional flows

    Basic flows -Source, Sink, Free and Forced vortex, uniform parallel flow. Their combinations,Pressure and velocity distributions on bodies with and without circulation in ideal and realfluid flows. Kutta Joukowski's theorem.

    Module 3.(10 hours)Conformal transformation

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    71/249

    Joukowski Transformation and its application to fluid flow problems, Kutta condition, Blasiustheorem.

    Module 4.(10hours)AIRFOIL AND WING THEORYJoukowski, Karman -Trefftz, Profiles -Thin aerofoil theory and its applications. Vortex line,Horse shoe vortex, Biot and Savart law, Lifting line theory and its limitations. viscous

    flow:Newton's law of viscosity, Boundary Layer, Navier-Stokes equation, displacement,Momentum thickness, Flow over a flat plate, Blasins solution.

    Text books

    Anderson, J.D., "Fundamentals of Aerodynamics", McGraw-Hill Book Co., New York, 1985

    References

    1. Houghton, E.L., and Carruthers, N.B., "Aerodynamics for Engineering students",

    Edward Arnold Publishers Ltd., London, 1989.2. Milne Thomson, L.H., "Theoretical aerodynamics", Macmillan, 1985.3. Clancey, L.J., "Aerodynamics", Pitman, 1986

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    72/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    73/249

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    74/249

    AN09 507(P) AIRCRAFT STRUCTURES LAB -II

    Teaching scheme Credits: 23 hours practical per week

    ObjectiveTo experimentally study the unsymmetrical bending of beams, find the location of shear

    centre, obtain the stresses in circular discs and beams using photo elastic techniques,calibration of photo -elastic materials and study on vibration of beams.

    List of experiments

    1. Unsymmetrical bending of beams2. Shear centre location for open sections3. Shear centre location for closed sections

    4. Constant strength beam5. Flexibility matrix for cantilever beam

    6. Beam with combined loading7. Calibration of Photo-elastic materials8. Stresses in circular discs and beams using photo elastic techniques9. Vibrations of beams10. Wagner beam -Tension field beam

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    75/249

    Internal Continuous Assessment (Maximum Marks-50)

    60% - Practicals and record (30 marks)

    30% - Test /s (15 marks)

    10% - Regularity in the class (5 marks)

    Semester End Examination (Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)20% - Viva voce (10 marks)10% - Fair record (5 marks)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    76/249

    AN09 508(P) AIRCRAFT STRUCTURES REPAIR AND

    MAINTENANCE LAB

    Teaching scheme Credits: 23 hours practical per week

    Objective:To give training on riveting, patchwork, welding and carpentry

    List of experiments

    I. Aircraft wood gluing1.Welded patch repair by TIG, MIG, PLASMA ARC.2.Welded patch repair by MIG3.Welded patch repair by plasma Arc4.Fabric Patch repair5.Riveted patch repairs.

    6.Repair of composites7.Repair of Sandwich panels.8.Sheet metal forming.9.Control cable inspection and repair.

    Internal Continuous Assessment(Maximum Marks-50)

    60% - Practicals and record (30 marks)30% - Test /s (15 marks)

    10% - Regularity in the class (5 marks)

    Semester End Examination (Maximum Marks-50)

    70% - Procedure, conducting experiment, results, tabulation, and inference (35 marks)

    20% - Viva voce (10 marks)10% - Fair record (5 marks)

  • 8/6/2019 B.TECH. AERONAUTICAL ENGINEERING Syllabus

    77/249

    VIth SEMESTER

    AN09 601 PROPULSION I

    Teaching scheme Credits: 5

    4 hours lecture and 1 hour tutorial per week

    ObjectiveTo understand the principles of operation and design of aircraft and spacecraft power plants.

    Module 1.(18hours)Fundamentals of gas turbine enginesIllustration of working of gas turbine engine -The thrust equation -Factors affecting thrust

    -Effect of pressure, velocity and temperature changes of air entering compressor -Methods of

    thrust augmentation Characteristics of turboprop, turbofan and turbojet -Performancecharacteristics.

    Module 2.(18hours)Subsonic and supersonic inlets for jet enginesInternal flow and Stall in subsonic inlets -Boundary layer separation -Major features ofexternal flow near a subsonic inlet -Relation between minimum area ratio and eternal

    deceleration ratio -Diffuser performance -Supersonic inlets -Starting problem on supersonicinlets -Shock swallowing by area variation -External declaration -Models of inlet operation.

    Module 3(16hours)Combustion chambers

    Classification of combustion chambers -Important factors affecting combustion chamberdesign Combustion process -Combustion chamber performance -Effect of operating variableson performance Flame tube cooling -Flame stabilization -Use of flame holders -Numericalproblems.

    Module 4. (20hours)NozzlesTheory of flow in isentropic nozzles -Convergent nozzles and nozzle choking -Nozzle throatconditions Nozzle efficiency -Losses in nozzles -Over expanded and under -expanded nozzles-Ejector and variable area nozzles -Interaction of nozzle flow with adjacent surfaces -Thrust

    reversal.

    Compressors

    Principle of operation of centrifugal compressor -Work done and pressure rise -Velocitydiagrams Diffuser vane design considerations


Top Related