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 50
... motion between the object and the fluid . If there is no motion , then there is no drag . It makes no difference whether the object moves through a static fluid or the fluid moves past a static solid object . Drag acts in a direction ...
... motion between the object and the fluid . If there is no motion , then there is no drag . It makes no difference whether the object moves through a static fluid or the fluid moves past a static solid object . Drag acts in a direction ...
Страница 72
... motion reduce to D = T L = W [ 4.11 ] [ 4.12 ] EXAMPLE 4.1 Equations of motion . JPG The thrust produced by the engine ( s ) exactly balances the drag , and the lift balances the weight . The performance of an airplane in steady , level ...
... motion reduce to D = T L = W [ 4.11 ] [ 4.12 ] EXAMPLE 4.1 Equations of motion . JPG The thrust produced by the engine ( s ) exactly balances the drag , and the lift balances the weight . The performance of an airplane in steady , level ...
Страница 147
... motion of the airplane is a response to these forces . In con- trast , airplane stability and control are governed by moments about the center of gravity , and the rotational motion of the plane is a response to these moments . Much of ...
... motion of the airplane is a response to these forces . In con- trast , airplane stability and control are governed by moments about the center of gravity , and the rotational motion of the plane is a response to these moments . Much of ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
21 други раздела не са показани
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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