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
... maximum camber in percent of the chord . The second digit represents where on the airfoil the maximum camber occurs , in tenths of the chord length aft of the leading edge . The third and fourth digits represent the maximum thickness in ...
... maximum camber in percent of the chord . The second digit represents where on the airfoil the maximum camber occurs , in tenths of the chord length aft of the leading edge . The third and fourth digits represent the maximum thickness in ...
Page 76
... maximum value . We saw that the maximum value of C is C , max ' the lift coefficient at stalling . The slowest speed at which an aircraft can fly in a straight and level flight is therefore called the stalling speed vstall . It is given ...
... maximum value . We saw that the maximum value of C is C , max ' the lift coefficient at stalling . The slowest speed at which an aircraft can fly in a straight and level flight is therefore called the stalling speed vstall . It is given ...
Page 81
... maximum range for a jet - powered aircraft is achieved when it flies such that C / C is a maximum . This condition can be restated in terms of L / D by using Equation ( 4.21 ) : L 2mg CL = = 2mg C / 2 PS Cn D PSCL CD [ 4.51 ] Hence we ...
... maximum range for a jet - powered aircraft is achieved when it flies such that C / C is a maximum . This condition can be restated in terms of L / D by using Equation ( 4.21 ) : L 2mg CL = = 2mg C / 2 PS Cn D PSCL CD [ 4.51 ] Hence we ...
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