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 152
... defined as [ 7.1 ] CM , ac = Mac 900 Sc [ 7.2 ] where q . is the dynamic pressure , S the wing area , and c the chord length . ( Recall the definition of the coefficient of lift and drag from Chapter 3 , " Aerodynamics . " ) The value ...
... defined as [ 7.1 ] CM , ac = Mac 900 Sc [ 7.2 ] where q . is the dynamic pressure , S the wing area , and c the chord length . ( Recall the definition of the coefficient of lift and drag from Chapter 3 , " Aerodynamics . " ) The value ...
Page 217
... defined as the equipment that performs the satellite mission function . For example , a telecommunication satel- lite's payload would be defined as the equipment that receives , processes , and transmits communication data . The ...
... defined as the equipment that performs the satellite mission function . For example , a telecommunication satel- lite's payload would be defined as the equipment that receives , processes , and transmits communication data . The ...
Page 319
... defined as the solid angle which , having its vertex in the center of the sphere , cuts off an area of the sphere ... Definition of the plane angle SI unit , radian , and the solid angle SI unit , steradian . 1 rad r Table A.2 | Derived ...
... defined as the solid angle which , having its vertex in the center of the sphere , cuts off an area of the sphere ... Definition of the plane angle SI unit , radian , and the solid angle SI unit , steradian . 1 rad r Table A.2 | Derived ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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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