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 88
... determined from v / r , which in this case turns out to be g ( 1 − n ) @ = ν [ 4.75 ] 4.5.2 The V - n Diagram Let us now determine the flight envelope of an aircraft , in other words the region where the aircraft operates in terms of ...
... determined from v / r , which in this case turns out to be g ( 1 − n ) @ = ν [ 4.75 ] 4.5.2 The V - n Diagram Let us now determine the flight envelope of an aircraft , in other words the region where the aircraft operates in terms of ...
Страница 127
... determines the temperature change . The energy output of the burner stage is desired . Since fuel is added in the burner ... determine the engine's specific fuel consumption . As explained in Chapter 4 , " Aircraft Performance , " the ...
... determines the temperature change . The energy output of the burner stage is desired . Since fuel is added in the burner ... determine the engine's specific fuel consumption . As explained in Chapter 4 , " Aircraft Performance , " the ...
Страница 133
... Determine the difference between the inlet and exit velocity . Ue - Uo = 4.8 × 107 J / kg 300 m / s -0.01 0.5 0.5 = 400 m / s Determine the thrust to mass flow times the velocity ratio . F muo = Ue Ио - 700 m / s 1 = 300 m / s 1 - 4 3 ...
... Determine the difference between the inlet and exit velocity . Ue - Uo = 4.8 × 107 J / kg 300 m / s -0.01 0.5 0.5 = 400 m / s Determine the thrust to mass flow times the velocity ratio . F muo = Ue Ио - 700 m / s 1 = 300 m / s 1 - 4 3 ...
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 |