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Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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AER 101 Introduction to AeronauticsInstructor : Prof. Dr. Galal Bahgat Salem
Textbook : John D. Anderson, Jr, Introduction to Flight , 4th Edition ,
2000.
Term Work : 25 +25 = 50 Marks
Final Exam: 50 +50 = 100 Marks
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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AER 101 A Introduction to Aeronautics ( 2 + 1 )
• History of Flight• Nature of Aerodynamic Forces• Airplane components and Configurations• Scope of Aeronautical Engineering• Fluid Properties and Characteristics• Atmosphere• Basic Aerodynamics : Kinematics, Continuity and
Bernoulli’s Equations, Boundary Layer Concept, Skin Friction, Pressure Drag, Flow Separation, Streamlining
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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AER 101B Introduction to Aeronautics ( 2 + 1 )
• Geometric and Aerodynamic Characteristics of Airfoils• Dimensional Analysis and Aerodynamic Force
Coefficients• Elements of Airplane Performance: Drag-Speed Curve,
Cruising Flight Performance, Climbing Performance, Gliding Performance
• Elements of Propulsion: Propellers, Piston Engines, Reaction Principle, Jet Engines, Rocket Motors
• Elements of Airplane Stability and Control
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Chapter 1History Of Flight
What is Flight ?
■ Flight is a motion in air free from ground topography
■ It is a high-speed motion through a low-resistance ( low density ) medium which is air
N.B. Compare flight in air, having a density of 1.225 Kg/m3, with shipping in water of density 1000 Kg/m3
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Short History of Flight1. Imitating Birds
• People attempting to fly by using artificial wings strapped to their arms and-or legs
• The flapping of wings generate lift• The Greek myth of Daedalus and his son Icarus
imprisoned on the island of Crete in the Mediterranean Sea illustrates man’s flight
• The idea of strapping a pair of wings to arms fell out of favor
• It was replaced by concept of wings flapped up and down by various mechanical devices,
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Powered by human arm, leg, or body movement• These are called Ornithopters • Ornithopters first designed by Leonardo da
Vinci ( 1452-1519 )
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Why Don’t Ornithopters Work?
• G. A. Borelli (1680 ) realized the fact that ( power/weight) ratio of a man is much less than that of bird
• Hence man will never be able to fly like a bird, by his own power only
2. Lighter-than-Air Balloons[Unpowered Flight]
● Firstly hot air balloons discovered by the Montgolfier Brothers in France (1783)
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• Later on gas balloons of Hydrogen/Helium were used by Charles
• Charles found that ballooning is based on Archimedes principle of buoyancy
• Unmanned Balloon Manned Balloon
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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3. Lighter-than-Air Dirigibles (Airships)[Powered]●Firstly invented by Count von Zeppelin in
Germany (1900) ●They are more rigid (the first airframe) than
balloons, controlled and directed (using stabilizing surfaces) and propeller droved
●Large bags of gas inside the rigid airframe●Count von Zeppelin (1929), flew around the world
in 21 days●Hydrogen fired in “Hindenburg” dirigible in 1937
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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4.Sir George Cayley (1799) ●First pioneered the concept for the modern airplane
configuration in 1799 - Fixed wings, tail, fuselage - Separate mechanism for propulsion “separation of lift and propulsion”● Recognized that the function of thrust was to overcome
aerodynamic drag ●Drew the first lift-drag vector diagram in the historyN.B. Before this time flapping wings were supposed to
provide both lift and propulsion
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Lift Resultant Aerodynamic
Force
Drag
Thrust
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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5.Heavier-than-Air Unpowered Gliders (Sailplanes)
• Gliders first designed and flew by Otto Lilienthal, a German mechanical engineer, in 1891
• Lilienthal is known as the glider’s man• Gliders characterized by un-sustained flight
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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He died in 1896, after stalling a glider he was flying
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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6.Heavier-than-Air Powered Airplanes
• Samuel P. Langley was contracted to build a flying machine for the U.S. government
• Began a series of aerodynamic experiments in 1887• Successful in flying several small scale, unmanned,
powered aircraft, which he called aerodromes• These were the first steam-powered, heavier-than-air
machines to successfully fly• Langley’s attempt to build a manned aerodrome failed• Lunched and crashed on Oct. 7 and December 8, 1903
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Langley’s aerodrome shortly after launch
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The Wright Brothers • Wright brothers (Orville&Wilbur) were the
inventors of the first practical manned flight on 17 Dec.,1903 (Flyer I )
• It was a strut-and-wire biplane configuration• Propulsion was achieved by a four-cylinder in-
line engine designed and built by Orville Wright• It produced close to 12 hp and weighed 140 Ibs• It drove two propellers via a bicycle-like chain
loop
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The control feature of Wright flyer is one of the basic reasons for its success
• Flyer I had a wing span of 12 m , flew a distance of 256 m, and lasting 59 sec
Wright Flyer Engine
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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■ Hydrostatics of Lighter-than-Air Flight
• The lifting force is the buoyancy force• The basic laws of hydrostatics (fluid at rest) are:
a- fluid pressure p is uniform in horizontal
planes, as well as the density
b- p varies only with height z according to the
Hydrostatic equation z
datum
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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dp/dz = -ρg
Integrating, in case of constant density:
p + ρ g z = constant
This is the hydrostatic equation
non-uniform
p distribution
on a body immersed
in a fluid at rest
p
p + ρ g z
z
B
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The resultant fluid-pressure force is called the buoyancy force B, acting vertically upward, and equals to the weight of the displaced fluid
• B = ρ g V
where ρ density of fluid
g acceleration of gravity
V volume of immersed body
N.B. The basis of Heavier-than-air Flight will discussed later
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Anatomy OF THE AIRPLANE
■The Main Components of the Airplane
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The basic airplane components include: fuselage, wing, tail assembly, control surfaces, landing gear, and power plant(s)
1.The Fuselage
♦ It carries the payload.
♦ It is the central structural member of the
airframe to which other members are attached.
♦ It is generally streamlined to reduce drag.
♦ Designs vary with the mission to be performed,
as illustrated in figure
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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2.The Wing
● It generates the lift force. • It includes the flaps for lift augmentation during
landing and takeoff, and ailerons for banking the airplane during turning.
• The wing cross-section is called Airfoil• The airfoil shape, wing planform shape, and
placement of the wing on the fuselage depend upon the airplane mission.
• The figure illustrates wing shapes and placements
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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3.Tail Assembly and Control Surfaces
• The tail assembly (empennage) represents the collection of structures at the rear of the airplane
• The tail assembly consists of:
1- The vertical stabilizer (fin) and rudder which
provide directional stability in yaw
2-The horizontal stabilizer and elevator which
provide longitudinal stability in pitch
● The figure illustrates different forms of tail assembly
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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4.Landing Gear
• The landing gear (undercarriage) supports the airplane while it is at rest on the ground and during the takeoff and landing
• The gear may be fixed or retractable• The wheels are attached to shock-absorbing
struts that use oil or air to cushion the blow of landing
• Special types of landing gear include skids for snow and floats for water
• For carrier landings, arrester hooks are used
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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4.Power Plants
• Power plants used to produce the thrust force necessary to propel the airplane to overcome the drag
• The power plant consists of the engine (and propeller, if present) and accessories
• The main engine types are:
-Reciprocating (or piston type)
-Reaction engines such as turbojet, turbofan, turboprop, ram jet, pulse jet, and rocket engine
The figure shows several some of engine placements
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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■The Aircraft Structure
• The figure shows a cutaway drawing of an aircraft structure
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Basic Elements of Aircraft Structure
■The wing
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• Wing structure basically same in all aircraft types
• Modern aircrafts have all metal and composite material wings but many older had wood and fabric wings
• The wing is a framework composed of spars, ribs and (possibly) stringers (see figure)
• Spars are the main members of the wing. They extended lengthwise of the wing (crosswise of fuselage)
• Most wing structures have two spars, the front spar and the rear spar
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• Front spar near the leading edge, while the rear spar at about two-thirds the distance to the trailing edge
• The ribs are the parts of the wing which support the covering and provide the airfoil shape
• A skin covers the wing framework
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The fuselage structural elements are:
1-Bulkheads, which form the cross-sectional shape of the fuselage
2-Longerons, which are heavy strips that run the length of the fuselage and are attached to the outer edge of the bulkheads
3-Fuselage skin, which is attached to the longerons
N.B. Keelson is a strong beam placed at the bottom of the fuselage. The keelson is frequently used in military fighter aircrafts
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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■ Aerodynamic Basis of Heavier-than-Air Flight
• This is the real flight• It needs a lifting force to balance the weight;
since the buoyancy force is not sufficient• The source of the lifting force is the fact that
when a fluid is in motion, its pressure varies not only with height, as in the case of rest, but also with its velocity
• The relation between p, V, and z is expressed by Bernoulli’ equation (1738) :
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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p + (1/2) ρ V2 + ρ gz = constant
• Where p static pressure
• (1/2) ρ V2 dynamic pressure
• ρ g z head pressure
• The shape of an airplane-wing cross section (known as aerofoil or airfoil) was evolved from the Venturi tube, as shown :
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• When a fluid flows over a body (or a surface), or when a body is forced to move through a fluid, the fluid velocity relative to the body surface may be increased or decreased (depending on surface shape and altitude)
• And consequently the fluid pressure p may decrease or increase according to Bernoulli’s equation
• The resultant will be a net fluid force F acting on the body which is completely different than the Buoyancy force (and may be many times greater than it)
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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How does an Airplane fly?
• The key to the generation of lift is the specially-designed streamlined body, called the wing, and characterized by a special cross-section, called airfoil
• When the wing is propelled through air at a suitable angle of attack, and with a relatively-high speed, the air flowing around its surface is accelerated and/or decelerated according to Bernoulli’s equation
• The integration of the air-pressure distribution over the surface of the wing results in a resultant aerodynamic force F
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• The component of R perpendicular to flight direction (direction of relative motion) is called the Lift L
• The component of R opposite to flight direction is called drag D
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Forces on an AirplaneBasically, the four forces acting on an airplane are
weight, thrust, lift, and drag
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• Weight: The weight includes the airplane itself, the payload, and the fuel. Since the fuel is consumed as the airplane flies, the weight decreases. Weight acts in a direction towards the center of the Earth.
• Thrust: The driving force of whatever propulsive system is used, engine driven propeller, jet engine, rocket engine, and so forth, is the thrust. It may be taken to act along the longitudinal axis of the airplane.
• Lift: This force is generated by the flow of air around the airplane, the major portion resulting from the wing. It represents the component of the resultant aerodynamic force normal to the flight direction.
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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• Drag: This force arises from the flow of air around the airplane and is the component of the resultant aerodynamic force opposite to the flight direction
• For un-accelerated (Steady) level flight:
L = W T = D
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Scope of Aerospace Engineering
• Aerospace engineering means airplane, missiles (Rockets), and satellite design, manufacturing, testing, maintaining, repairing, overhauling, and performance analysis
▄ The Main Topics A.E. are: (1) Aerodynamics (2) Airframe Design (3) Propulsion (4) Flight Mechanics & Control
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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■ The Associated Topics are: ►Flight navigation ►Electronics ( + Flight navigation = Avionics ) ►Meteorology ►Metallurgy ►Production Engineering ►Fluid-power engineering (pneumatic, hydraulic, pressurization, and air-conditioning systems) ►Instrumentation ►Chemical & fuel engineering ►Flight regulations & Airworthiness
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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■ The Associated Topics are: ►Flight navigation ►Electronics ( + Flight navigation = Avionics ) ►Meteorology ►Metallurgy ►Production Engineering ►Fluid-power engineering (pneumatic, hydraulic, pressurization, and air-conditioning systems) ►Instrumentation ►Chemical & fuel engineering ►Flight regulations & Airworthiness
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Aerodynamics
●Aerodynamic design of the flight vehicle/space vehicle for:
►Maximum lift production ►Minimum drag ►Max. available space for structure and payload●Determination of the aerodynamic forces on the
designed configuration at the different flight conditions (speed, attitude, and a altitude)
● Wind-tunnel testing●Flight testing
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Propulsion
●Power-plant design & construction for:
►Max. thrust/weight of engine
►Max. thrust/drag of engine
►Min. specific fuel consumption (sfc)
►Good performance at different altitudes and speeds of flight
●Power-plant manufacturing
●Power-plant testing
Prof. Galal Bahgat Salem Aerospace Dept., Cairo University
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Airframe Design
●Structural analysis
●Airframe design & construction for: sufficient strength and with less weight
●Airframe manufacturing techniques
●Airframe testing techniques