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 58
... camber , its point of maximum camber located at its 40 percent chord point , and a maximum thickness at 12 percent of its chord length . 3.4 3.4.1 SIMULATION FoilSim The FoilSim computer program developed by NASA provides an excellent ...
... camber , its point of maximum camber located at its 40 percent chord point , and a maximum thickness at 12 percent of its chord length . 3.4 3.4.1 SIMULATION FoilSim The FoilSim computer program developed by NASA provides an excellent ...
Page 62
... camber at 0. Record lift . Increase camber to 0.25 , 0.30 , 0.35 , 0.40 , 0.45 , and 0.50 , and record the changes in lift for each setting . Graph camber versus lift with the data recorded . Is it possible for camber adjustment to ...
... camber at 0. Record lift . Increase camber to 0.25 , 0.30 , 0.35 , 0.40 , 0.45 , and 0.50 , and record the changes in lift for each setting . Graph camber versus lift with the data recorded . Is it possible for camber adjustment to ...
Page 63
... camber as a percentage of the chord . The second integer indicates the position of the maximum camber in terms of tenths of the chord length measured from the leading edge . The last two integers indicate the thickness of the airfoil as ...
... camber as a percentage of the chord . The second integer indicates the position of the maximum camber in terms of tenths of the chord length measured from the leading edge . The last two integers indicate the thickness of the airfoil as ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing