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 73
... calculated for any aircraft as follows : 1. Determine the air density p from the standard atmosphere for a given alti- tude h . 2. Calculate the lift coefficient C , for a given velocity v , by recalling the def- inition of dynamic ...
... calculated for any aircraft as follows : 1. Determine the air density p from the standard atmosphere for a given alti- tude h . 2. Calculate the lift coefficient C , for a given velocity v , by recalling the def- inition of dynamic ...
Страница 93
... calculate the speed of sound , then calculate velocity . The aspect ratio of the aircraft , fuel mass , and aircraft mass can then be calculated . Finally , calculate range and endurance , using the coefficients of lift and drag ...
... calculate the speed of sound , then calculate velocity . The aspect ratio of the aircraft , fuel mass , and aircraft mass can then be calculated . Finally , calculate range and endurance , using the coefficients of lift and drag ...
Страница 266
... calculations . Table 11.3 also reveals the design specification of the EMU . From the past discussion it is easy to ... calculated [ N ( lb ) ] Force design [ N ( lb ) ] Finger 2.5 ( 1 ) 5.1 ( 2 ) 7.6 ( 1.7 ) Human capability [ N ( lb ) ...
... calculations . Table 11.3 also reveals the design specification of the EMU . From the past discussion it is easy to ... calculated [ N ( lb ) ] Force design [ N ( lb ) ] Finger 2.5 ( 1 ) 5.1 ( 2 ) 7.6 ( 1.7 ) Human capability [ N ( lb ) ...
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 |