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 132
... engine manufacturer . We now know all the necessary relations between gas turbine engine com- ponents to solve for the thrust developed by the jet engine . Given that the EPR , the inlet losses , and the corresponding engine temperature ...
... engine manufacturer . We now know all the necessary relations between gas turbine engine com- ponents to solve for the thrust developed by the jet engine . Given that the EPR , the inlet losses , and the corresponding engine temperature ...
Страница 141
... engine to achieve the greatest thrust pos- sible in the shortest time . In other words , the engine must burn a large mass of fuel and push the resulting gas out of the engine as rapidly as possible . Newton's second law of motion can ...
... engine to achieve the greatest thrust pos- sible in the shortest time . In other words , the engine must burn a large mass of fuel and push the resulting gas out of the engine as rapidly as possible . Newton's second law of motion can ...
Страница 143
... engines of the Space Shuttle era include those that have propelled NASA's Shuttle and the Russian's Buran reusable space vehicles into orbit . The X - 1 used a rocket engine to become the first aircraft to reach supersonic flight ...
... engines of the Space Shuttle era include those that have propelled NASA's Shuttle and the Russian's Buran reusable space vehicles into orbit . The X - 1 used a rocket engine to become the first aircraft to reach supersonic flight ...
Съдържание
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
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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