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 52
... coefficient . The important point is this : It is completely incorrect to measure a drag coefficient at some low speed ( say , 200 mph ) and apply that drag coefficient at twice the speed of sound ( approximately 1,400 mph , M = 2.0 ) ...
... coefficient . The important point is this : It is completely incorrect to measure a drag coefficient at some low speed ( say , 200 mph ) and apply that drag coefficient at twice the speed of sound ( approximately 1,400 mph , M = 2.0 ) ...
Page 56
... coefficient of drag as CD . Finally , the total drag coefficient becomes CDTOTAL = CD2 + C TEAR [ 3.34 ] Figure 3.5 gave the overall shape of coefficient of lift and coefficient of drag curves as a function of airfoil angle of attack ...
... coefficient of drag as CD . Finally , the total drag coefficient becomes CDTOTAL = CD2 + C TEAR [ 3.34 ] Figure 3.5 gave the overall shape of coefficient of lift and coefficient of drag curves as a function of airfoil angle of attack ...
Page 336
... coefficient , moment , 152 , 153 coefficient , solar absorption , 167–69 coefficient , specific heat , 127 coefficient of drag , 42 , 48 , 52 total , 56 coefficient of lift defined , 42 , 48 equation , 75 and flight envelope , 89 and ...
... coefficient , moment , 152 , 153 coefficient , solar absorption , 167–69 coefficient , specific heat , 127 coefficient of drag , 42 , 48 , 52 total , 56 coefficient of lift defined , 42 , 48 equation , 75 and flight envelope , 89 and ...
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