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 . 6.6 ...
... 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 . 6.6 ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
21 други раздела не са показани
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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
Библиография
| Заглавие | Interactive Aerospace Engineering and Design Aeronautical and Aerospace Engineering Series McGraw-Hill series in aeronautical and aerospace engineering Regulatory Manual Series |
| Автор | Dava J. Newman |
| Издание | илюстрирано |
| Издател | McGraw-Hill, 2002 |
| Оригиналът е от | Мичиганският университет |
| Цифровизирана на | 14 Дек 2007 |
| ISBN | 0072348208, 9780072348200 |
| Брой страници | 356 страници |
| Експортиране на описанието | BiBTeX EndNote RefMan |