Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници This text contains an integrated bound-in CD-ROM, and has a strong emphasis on design. Its active visual approach and inclusion of space-orientated engineering make it an interesting examination of the aerospace engineering field. |
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Страница 40
... called the leading edge ; the back of the wing is called the trailing edge . The distance from the leading to trailing edges is called the chord c . The ends of the wing are called the wing tips , and the distance from one wing tip to ...
... called the leading edge ; the back of the wing is called the trailing edge . The distance from the leading to trailing edges is called the chord c . The ends of the wing are called the wing tips , and the distance from one wing tip to ...
Страница 41
... called an airfoil , and it has some geometric definitions of its own , as shown to the left on the figure . The chord line has already been defined , and it cuts the airfoil into an upper surface and a lower surface . If we plot the ...
... called an airfoil , and it has some geometric definitions of its own , as shown to the left on the figure . The chord line has already been defined , and it cuts the airfoil into an upper surface and a lower surface . If we plot the ...
Страница 68
... called the rudder . Unlike the other two control elements ( i.e. , ailerons and elevators ) , a deflection of the rudder is made by the pilot not with his or her hands deflecting the control column but rather with his or her feet using ...
... called the rudder . Unlike the other two control elements ( i.e. , ailerons and elevators ) , a deflection of the rudder is made by the pilot not with his or her hands deflecting the control column but rather with his or her feet using ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
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aerodynamic aerospace aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere balloon body calculated CD-ROM chapter coefficient components compressor crew member Decavitator defined density design process drag drawing ellipse energy Equation example Figure flight force fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift lines low Earth orbit LTA vehicle lunar magnetic field magnetosphere maneuver materials maximum microgravity mission module motion multiview NASA nozzle object onboard operational orbital mechanics oxygen parameters particles payload percent performance plane planetary pressure problem propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight spacesuit design specific speed stability structural subsystem surface temperature thermal thrust turbine units Van Allen belts vector vehicle design velocity wing