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 73
... thrust required , and the thrust available . We assume that the thrust available exceeds the thrust required and that the thrust produced by the engines is exactly as much as is required . Hence , the thrust required for steady ...
... thrust required , and the thrust available . We assume that the thrust available exceeds the thrust required and that the thrust produced by the engines is exactly as much as is required . Hence , the thrust required for steady ...
Page 74
... thrust available decreases approximately linearly with increasing speed . For the jet engine example above , we assumed the engines put out thrust available over the entire operating range of aircraft velocities , which is reasonable ...
... thrust available decreases approximately linearly with increasing speed . For the jet engine example above , we assumed the engines put out thrust available over the entire operating range of aircraft velocities , which is reasonable ...
Page 135
... thrust equation given in Equation ( 6.1 ) contains two interesting terms . Aerospace engineers often refer to the first term ( exit mass flow rate times exit velocity ) as the gross thrust since this term is mostly associated with ...
... thrust equation given in Equation ( 6.1 ) contains two interesting terms . Aerospace engineers often refer to the first term ( exit mass flow rate times exit velocity ) as the gross thrust since this term is mostly associated with ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
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