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 50
... surface of the aircraft . Because the skin friction is an interaction between a solid and a gas , the magnitude of the skin friction depends on the properties of both . For the solid , a smooth , waxed surface produces less skin ...
... surface of the aircraft . Because the skin friction is an interaction between a solid and a gas , the magnitude of the skin friction depends on the properties of both . For the solid , a smooth , waxed surface produces less skin ...
Page 52
... surface . This shear stress can be written as a function of the Reynolds number [ recall Equation ( 3.21 ) ] : Re = ∞ Poovoot M∞o The shear stress on the lifting surface 7 is written as T = 0.664q . V Re [ 3.23 ] as a function of the ...
... surface . This shear stress can be written as a function of the Reynolds number [ recall Equation ( 3.21 ) ] : Re = ∞ Poovoot M∞o The shear stress on the lifting surface 7 is written as T = 0.664q . V Re [ 3.23 ] as a function of the ...
Page 190
... surface . Finding ( and utilizing ) this ice is a future goal for exploration missions [ 66 ] . As shown by the Pathfinder spacecraft , the Mars surface is diverse . Mars sees winds blowing from all directions within a single Sol , with ...
... surface . Finding ( and utilizing ) this ice is a future goal for exploration missions [ 66 ] . As shown by the Pathfinder spacecraft , the Mars surface is diverse . Mars sees winds blowing from all directions within a single Sol , with ...
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