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Introduction to Aerospace Engineering Octavian Thor Pleter, PhD, PhD, MBA (MBS) 1 IAEC02 This presentation draws on ideas from Dr. Pleter’s articles, books, and unpublished manuscripts. No part of this publication may be reproduced, stored in a retrieval system or transmitted by any means or in any form - electronic, mechanical, photocopying, recording or otherwise - without written consent from Octavian Thor Pleter or the Brainbond consultancy firm, www.brainbond.ro Version 1.0 dated 23 October 2009 © O. T. Pleter and Brainbond
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  • Introduction to Aerospace Engineering

    Octavian Thor Pleter, PhD, PhD, MBA (MBS)

    1 IAEC02

    This presentation draws on ideas from Dr. Pleters articles, books, and unpublished manuscripts. No part of this publication may be reproduced, stored in a retrieval system or transmitted by any means or in any form - electronic,

    mechanical, photocopying, recording or otherwise - without written consent from Octavian Thor Pleter or the

    Brainbond consultancy firm, www.brainbond.ro Version 1.0 dated 23 October 2009 O. T. Pleter and Brainbond

  • Course Outlines

    1. Introduction. Why Aerospace Engineering?

    2. Flight Principles. Classification of Aircraft and Spacecraft.

    3. Airplane. Aircraft Structure and Systems. Flight Control.

    4. Aircraft Classes and Categories. Aircraft Materials.

    5. Airplane Flight. Lift, Weight, Thrust, Drag. Airfoils.

    6. Axes. Controls, Stability. Load Factor. Stall.

    7. Helicopters. Controls, Stability. Lighter than Air Aircraft.

    8. Airspeed, Mach Number. Flight Instruments: Pitot, Gyro, Magnetic.

    9. Aero Engines and the Fuel System. Piston Engine. Jet Engine.

    Instruments.

    10.Aerodrome Operations. Air Traffic Management, Airspace. VFR, IFR.

    11.Spacecraft Propulsion, Control and Stability.

    12.Navigation. Air Navigation Systems. Automatic Flight Control. FMS.

    13.Air Transport Engineering. Aviation Business. Regulators. Chicago

    Convention.

    14.Conclusions.

    2 IAEC02

  • I. Every object in a state of uniform motion tends to

    remain in that state of motion unless an external

    force is applied to it.

    3 IAEC02

    Newtons Laws

    II. The relationship between an object's mass m, its

    acceleration a, and the applied force F is F = ma.

    III. For every action there is an equal and opposite

    reaction.

  • 4 IAEC02

    Flight

    Non-atmospheric

    flight: does not

    require the

    atmosphere to lift

    the body

    Atmospheric flight: requires

    the atmosphere

    (a fluid) to lift

    the body

    atmosphere acts

    like a break; may

    be used to steer

    the vehicle

  • 5 IAEC02

    Flight

    Non-Atmospheric

    Flight

    Atmospheric

    Aerodynamic Lift

    Flight

    Ballistic Flight Heavier-than-Air Flight

    Reaction Flight Lighter-than-Air Flight

  • 6 IAEC02

    Non-Atmospheric Flight

  • The bullet keeps its motion after launch, on a straight trajectory.

    Gravity will eventually bring it down (Newtons 2nd). Friction with air will slow it down (Newtons 2nd). The launch mechanics: explosion exhaust gas is pushed back bullet is pushed forward (Newtons 3rd).

    7 IAEC02

    Ballistic Flight - Newtons 1st

  • V1 = 7.82 km/s

    Defeat gravity by centrifugal force.

    Avoid friction with air extra-atmospheric flight.

    8 IAEC02

    Spacecraft in Earth Orbit = Ballistic Flight at 1st Cosmic Speed

  • The launch mechanics:

    violent burn of rocket fuel

    exhaust gas is pushed down

    rocket is pushed up (Newtons 3rd).

    go vertically to get rid of the atmosphere

    then go tangentially to V1 to defeat gravity

    9 IAEC02

    Spacecraft in Earth Orbit = Ballistic Flight at 1st Cosmic Speed

  • IAEC02 10

  • G = 6.6726 x 10-11 m3/kg/s2

    - the universal constant of gravitation

    M = 5.98 x 1024 kg mass of the Earth

    11 IAEC02

    Spacecraft in Earth Orbit = Ballistic Flight at 1st Cosmic Speed

    2

    2

    V mMm G

    R R

    GMV

    R

  • RE = 6,371 km

    ALT = 400 km

    V = ?

    12 IAEC02

    Problem: the International Space Station

    GMV

    R

    G = 6.6726 x 10-11 m3/kg/s2

    - the universal constant of gravitation

    M = 5.98 x 1024 kg Earth mass

  • V = 7.676 km/s = 27,600 km/h

    13 IAEC02

    Problem: the International Space Station

    GMV

    R

  • R = 6,371 km

    ALT = 20,200 km

    V = ?

    14 IAEC02

    Problem: GPS satellite velocity

    G = 6.6726 x 10-11 m3/kg/s2

    - the universal constant of gravitation

    M = 5.98 x 1024 kg mass of the Earth

  • Rocket launch:

    violent burn of rocket fuel

    exhaust gas is pushed down

    rocket is pushed up (Newtons 3rd)

    15 IAEC02

    Newtons 3rd Reaction Flight

  • Manned Spacecraft

    16 IAEC02

    Spacecraft

    Soyuz

  • Unmanned Spacecraft

    17 IAEC02

    Spacecraft

    Voyager

  • Space Shuttle

    18 IAEC02

    Spacecraft

    Reusable Manned

    Spaceship

    capable of landing

    after gliding in the

    atmosphere

  • Multi-stage Liquid Fuel Rocket

    19 IAEC02

    Launch Rockets

    Saturn V

  • 20 IAEC02

    Atmospheric Aerodynamic Lift Flight

  • How do the birds fly?

    21 IAEC02

  • Bird flying:

    wings push the air down

    bird is pushed up (Newtons 3rd)

    22 IAEC02

    Newtons 3rd Heavier-than-Air Atmospheric Flight

  • Newtons 3rd Lighter-than-Air Atmospheric Flight

    23 IAEC02

    Atmosphere =

    Fluid

  • 24 IAEC02

    Archimedes Principle

    Any object, wholly or

    partly immersed in a

    fluid, is buoyed up

    by a force equal to

    the weight of the

    fluid displaced by

    the object."

  • Balloon

    25 IAEC02

    ( )gasW m V g

    airL V g Gas Density

    kg/m3 *)

    Air 1.204

    Helium (He) 0.1786

    Hydrogen (H) 0.0899

    *) in normal conditions:

    +20C at sea level

  • IAEC02 26

    Rescuers find helium balloons belonging to

    missing Brazilian priest floating in the sea

    Last updated at 16:03 23 April 2008

    A Roman Catholic priest who went missing in

    seas off Brazil after trying to break a record for

    flying with helium balloons was today feared

    dead.

    Adelir Antonio de Carli is thought to have been

    blown 30 miles offshore after lifting off on Sunday

    afternoon.

    Today rescuers reached a cluster of brightly

    coloured party balloons floating in the ocean off

    Brazil's coast but did not find the priest.

  • 27 IAEC02

    Problem: Helium Balloons

    m = 80 kg (priest) + 20 kg (equipment) = 100 kg

    R = 0.4 m (balloon radius)

    How many Helium balloons are

    Needed to lift the priest?

    34

    3V R

  • 28 IAEC02

    Problem: Helium Balloons

    m = 80 kg (priest) + 20 kg (equipment) = 100 kg

    R = 0.4 m (balloon radius)

    How many Helium balloons are

    Needed to lift the priest?

    Vbal = 0.268 m3

    V = 97.5 m3

    N = V / Vbal = 364

    ! After liftoff the air density goes down

    34

    3balV R

    air He

    mV

  • Balloon

    29 IAEC02

    Lighter-than-Air Aircraft = Aerostats

    Free / Captive

    Hot Air / Helium

    Not Steerable

  • Airship (Dirigible)

    30 IAEC02

    Hydrogen / Helium

    Steerable

    Lighter-than-Air Aircraft = Aerostats

  • Kite

    31 IAEC02

    Heavier-than-Air Aircraft = Aerodynes

    Captive

  • Paraglider

    32 IAEC02

    Aerodynes

    Aerodynamic lift

    Non-powered

    foot-launched

    aircraft

  • Glider

    33 IAEC02

    Aerodynes

    Aerodynamic lift

    Non-powered

    Aircraft

  • Ultralight Aircraft (ULM)

    34 IAEC02

    Aerodynes

    Aerodynamic lift

    Powered Aircraft

    Under 300 kg

  • Fixed-Wing Land Aircraft

    35 IAEC02

    Aerodynes

    Aerodynamic lift

    Powered Aircraft

    Over 300 kg

    Uses land airfields

  • VTOL Aircraft

    36 IAEC02

    Aerodynes

    Vertical Take-off

    and Landing fixed

    wing aircraft with

    vectored

    propulsion

  • UAV Aircraft

    37 IAEC02

    Aerodynes

    Unmanned Air

    Vehicle

  • UCAV Aircraft

    38 IAEC02

    Aerodynes

    Unmanned

    Combat Air

    Vehicle;

    Unlike UAVs,

    UCAVs carry

    weapons

  • Hydroplanes (Seaplanes)

    39 IAEC02

    Aerodynes

    Aerodynamic lift

    Fixed-Wing Powered

    Aircraft

    Uses water to take-off

    and land

  • Fixed-Wing Amphibians

    40 IAEC02

    Aerodynes

    Aerodynamic lift

    Powered Aircraft

    Uses either water or

    land to take-off and land

  • Rotorcraft - Helicopters

    41 IAEC02

    Aerodynes

    Aerodynamic lift produced

    by a powered horizontal

    propeller (rotating wing)

  • Rotorcraft - Gyrodynes

    42 IAEC02

    Aerodynes

    Aerodynamic lift produced

    by a non-powered

    horizontal propeller

    (rotating wing)

    Horizontal thrust

  • Rotorcraft - Tiltrotor

    43 IAEC02

    Aerodynes

    Takes off like a helicopter

    Flies like a fixed-wing

    airplane

    Wing and Propellers tilt