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 4
... means of generating lift from the means of generating propulsion . In 1799 , he designed an airplane that featured fixed wings for generating lift , paddles for propulsion , and a tail unit with horizontal and ver- tical stabilizers ...
... means of generating lift from the means of generating propulsion . In 1799 , he designed an airplane that featured fixed wings for generating lift , paddles for propulsion , and a tail unit with horizontal and ver- tical stabilizers ...
Страница 41
... mean camber line . For a symmetric airfoil that has an upper surface the same shape as the lower surface , the mean ... means high curvature ) . The maximum distance between the upper and lower surfaces is called the thickness . Often ...
... mean camber line . For a symmetric airfoil that has an upper surface the same shape as the lower surface , the mean ... means high curvature ) . The maximum distance between the upper and lower surfaces is called the thickness . Often ...
Страница 117
... means by which to achieve motion , a way to thrust themselves to accelerate and then counteract frictional forces from motion . In this process , an engine converts potential energy to kinetic energy and also replenishes the kinetic ...
... means by which to achieve motion , a way to thrust themselves to accelerate and then counteract frictional forces from motion . In this process , an engine converts potential energy to kinetic energy and also replenishes the kinetic ...
Съдържание
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Авторско право | |
15 други раздела не са показани
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aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing