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 58
... percent of the chord length ( 1 to 99 percent ) . The charts always show the lift curve as the left panel and the drag polar and moment polar ( C , and CM versus C1 ) as the right panel . A schematic of the airfoil is drawn in the top ...
... percent of the chord length ( 1 to 99 percent ) . The charts always show the lift curve as the left panel and the drag polar and moment polar ( C , and CM versus C1 ) as the right panel . A schematic of the airfoil is drawn in the top ...
Страница 190
... percent ) and argon ( 1.6 percent ) . Oxygen makes up only 0.13 percent of the Martian atmosphere . Clouds are rarely seen in Mars ' sky , as the amount of water vapor is 25 percent that of Earth . It is thought that this amount ...
... percent ) and argon ( 1.6 percent ) . Oxygen makes up only 0.13 percent of the Martian atmosphere . Clouds are rarely seen in Mars ' sky , as the amount of water vapor is 25 percent that of Earth . It is thought that this amount ...
Страница 255
... percent of the time the maximum force magnitude was below 90 N. For 95 percent of the astronaut motions , the root mean square force level was below 9.0 N. An analysis of the torques recorded showed that 99 percent of all events were ...
... percent of the time the maximum force magnitude was below 90 N. For 95 percent of the astronaut motions , the root mean square force level was below 9.0 N. An analysis of the torques recorded showed that 99 percent of all events were ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
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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