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 166
... density at a given altitude ( see Section 8.4.1 , " Solar Activity and Emissions , " for details ) . The same effects - inflation and variation of density - are observed to a lesser extent in a day - night cycle . One way to think about ...
... density at a given altitude ( see Section 8.4.1 , " Solar Activity and Emissions , " for details ) . The same effects - inflation and variation of density - are observed to a lesser extent in a day - night cycle . One way to think about ...
Страница 223
... density compared to an omnidirectional design . For example , in Figure 10.3 , the highly directional antenna is able to create a beam whose power is spread over one - fifth the surface area of a sphere at a radius R. An omnidirec ...
... density compared to an omnidirectional design . For example , in Figure 10.3 , the highly directional antenna is able to create a beam whose power is spread over one - fifth the surface area of a sphere at a radius R. An omnidirec ...
Страница 324
... Density P 1.161 x 10-3 kg / m3 Specific heat capacity at constant pressure Cp 1,003.5 J / ( kg K ) • Specific heat capacity at constant volume Cv 716.5 J / ( kg⚫K ) Ratio of specific heat capacities 1.4006 Specific gas constant R 287 J ...
... Density P 1.161 x 10-3 kg / m3 Specific heat capacity at constant pressure Cp 1,003.5 J / ( kg K ) • Specific heat capacity at constant volume Cv 716.5 J / ( kg⚫K ) Ratio of specific heat capacities 1.4006 Specific gas constant R 287 J ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
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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