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 65
... PARAMETERS There are many possible measures for aircraft performance . While some apply for all aircraft , others are specific to a certain type . The most common perfor- mance parameters , applicable to all types of airplanes , include ...
... PARAMETERS There are many possible measures for aircraft performance . While some apply for all aircraft , others are specific to a certain type . The most common perfor- mance parameters , applicable to all types of airplanes , include ...
Page 81
... parameters further , starting with the mass ratio . A large mue / mo can be obtained through proper selection of ... parameters in Table 4.4 . Table 4.4 | Designing for a large L / D ratio L / D design parameters High aspect ratio Smooth ...
... parameters further , starting with the mass ratio . A large mue / mo can be obtained through proper selection of ... parameters in Table 4.4 . Table 4.4 | Designing for a large L / D ratio L / D design parameters High aspect ratio Smooth ...
Page 347
... parameters 4. See bank angle paints absorptivity , 169 ( table ) , 227 ( table ) infrared emissivity , 169 ( table ) Pan Am , 8 parabola , 202 , 210 parabolic flight , 275 paraline images , 288 parameter , 211 , 212–13 parametric ...
... parameters 4. See bank angle paints absorptivity , 169 ( table ) , 227 ( table ) infrared emissivity , 169 ( table ) Pan Am , 8 parabola , 202 , 210 parabolic flight , 275 paraline images , 288 parameter , 211 , 212–13 parametric ...
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