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 47
... velocity is set to the velocity necessary for particles to separate , or detach , at the leading edge and meet at the trailing edge of the airfoil . The best way to under- stand the velocity variation is to use Newton's theory and ...
... velocity is set to the velocity necessary for particles to separate , or detach , at the leading edge and meet at the trailing edge of the airfoil . The best way to under- stand the velocity variation is to use Newton's theory and ...
Page 73
... velocity v . The relationship between the required thrust and the velocity can be calculated for any aircraft as follows : 1. Determine the air density p from the standard atmosphere for a given alti- tude h . 2. Calculate the lift ...
... velocity v . The relationship between the required thrust and the velocity can be calculated for any aircraft as follows : 1. Determine the air density p from the standard atmosphere for a given alti- tude h . 2. Calculate the lift ...
Page 74
... Velocity Curve Calculator V ( m / s ) 99 T = 62700 N him 145 S ( m2 ) 7.67 R 186825 ( N ) 5000 Jet Propeller Boeing ... velocity and altitude . There is a crossover velocity where diminishing thrust available and increasing thrust ...
... Velocity Curve Calculator V ( m / s ) 99 T = 62700 N him 145 S ( m2 ) 7.67 R 186825 ( N ) 5000 Jet Propeller Boeing ... velocity and altitude . There is a crossover velocity where diminishing thrust available and increasing thrust ...
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