Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pages 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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Page 117
... propulsion systems require a source of power and the means for accelerating airflow . The three primary sources of power or energy for propulsion are □ Hydrocarbon fuels and a heat engine . Batteries and an electric motor . Solar cells ...
... propulsion systems require a source of power and the means for accelerating airflow . The three primary sources of power or energy for propulsion are □ Hydrocarbon fuels and a heat engine . Batteries and an electric motor . Solar cells ...
Page 118
... propulsion systems develop thrust in dif- ferent ways , although it is usually generated through some application of ... Propulsion The details of propeller propulsion are complicated , but fundamental insights can be gleaned from ...
... propulsion systems develop thrust in dif- ferent ways , although it is usually generated through some application of ... Propulsion The details of propeller propulsion are complicated , but fundamental insights can be gleaned from ...
Page 144
... propulsion ? Why is this such a necessary characteristic ? 6.2 What kind of propulsion system does the Space Shuttle use , as opposed to an airplane ? 6.3 Jet engine certification . What is the first step in preparing a properly ...
... propulsion ? Why is this such a necessary characteristic ? 6.2 What kind of propulsion system does the Space Shuttle use , as opposed to an airplane ? 6.3 Jet engine certification . What is the first step in preparing a properly ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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Expressions et termes fréquents
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