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 41
... measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings have long spans ( like high - performance gliders ) while low ...
... measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings have long spans ( like high - performance gliders ) while low ...
Страница 231
... measurement unit ( IMU ) . The motion of the satellite can be measured with respect to a stabilized gyroscopic unit carried onboard . These are available for almost any mission ; however , the drift of the gyroscope associated with ...
... measurement unit ( IMU ) . The motion of the satellite can be measured with respect to a stabilized gyroscopic unit carried onboard . These are available for almost any mission ; however , the drift of the gyroscope associated with ...
Страница 237
... measurements are subtracted from the satellite position , resulting in a precise height measure- ment of the ocean above the geocenter , which is the sea level . The satellite meas- urement system is shown on the CD - ROM . Landsat 7 ...
... measurements are subtracted from the satellite position , resulting in a precise height measure- ment of the ocean above the geocenter , which is the sea level . The satellite meas- urement system is shown on the CD - ROM . Landsat 7 ...
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 |