Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pages 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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Page 63
... altitude with the data collected above , and predict the next two points on the graph . Is lift affected by an increase in altitude ? List possible reasons for any changes observed . ( f ) An airplane is beginning its descent at an ...
... altitude with the data collected above , and predict the next two points on the graph . Is lift affected by an increase in altitude ? List possible reasons for any changes observed . ( f ) An airplane is beginning its descent at an ...
Page 165
... altitude of 50 km . Here , the temperature gradient reverses , and the air actually gets warmer . At 18 km the temperature is about 220 K and rises to about 270 K ( -3 ° C ) at 50 km . This higher temperature results from heating via ...
... altitude of 50 km . Here , the temperature gradient reverses , and the air actually gets warmer . At 18 km the temperature is about 220 K and rises to about 270 K ( -3 ° C ) at 50 km . This higher temperature results from heating via ...
Page 173
... altitude ) . By flying in an orbit close to Earth , astronauts avoid strong doses of radiation that result from flying in high - altitude orbits . Even in LEO , satellites pass through the Van Allen belts , which are a source of heavy ...
... altitude ) . By flying in an orbit close to Earth , astronauts avoid strong doses of radiation that result from flying in high - altitude orbits . Even in LEO , satellites pass through the Van Allen belts , which are a source of heavy ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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Expressions et termes fréquents
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