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 41
... ratio is a measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings have long spans ( like high - performance gliders ) ...
... ratio is a measure of how long and slender a wing is from tip to tip . For a rectangular wing this reduces to the ratio of the span to the chord length . High - aspect - ratio wings have long spans ( like high - performance gliders ) ...
Page 81
... ratio . A large mue / mo can be obtained through proper selection of aircraft structures , materials , and overall design , as shown in Table 4.3 . Table 4.3 | Designing for a large mass ratio Mass ratio mtuel / mo Efficient structure ...
... ratio . A large mue / mo can be obtained through proper selection of aircraft structures , materials , and overall design , as shown in Table 4.3 . Table 4.3 | Designing for a large mass ratio Mass ratio mtuel / mo Efficient structure ...
Page 132
... ratio f [ given in Equation ( 6.16 ) ] . The equation for the exit velocity was developed in Section 6.3.6 , " Nozzles , " and depends on the thermodynamic properties of total temper- ature in the nozzle and the nozzle pressure ratio ...
... ratio f [ given in Equation ( 6.16 ) ] . The equation for the exit velocity was developed in Section 6.3.6 , " Nozzles , " and depends on the thermodynamic properties of total temper- ature in the nozzle and the nozzle pressure ratio ...
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