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 130
... nozzle . 6.3.6 Nozzles The gas turbine engine nozzle has three functions : to produce thrust , to conduct the exhaust gases back to the freestream , and to set the mass flow rate through the engine . See Figure 6.7 . The nozzle sits ...
... nozzle . 6.3.6 Nozzles The gas turbine engine nozzle has three functions : to produce thrust , to conduct the exhaust gases back to the freestream , and to set the mass flow rate through the engine . See Figure 6.7 . The nozzle sits ...
Page 131
... nozzle makes the aircraft much more maneuverable . The nozzle produces the thrust and also sets the total mass flow rate through the engine . The nozzle does no work on the flow ; nonetheless , there are some important design features ...
... nozzle makes the aircraft much more maneuverable . The nozzle produces the thrust and also sets the total mass flow rate through the engine . The nozzle does no work on the flow ; nonetheless , there are some important design features ...
Page 132
... nozzle efficiency , which is normally very close to 1 . [ 6.25 ] The nozzle performance equations work just as well for rocket engines except that rocket nozzles always expand the flow to some supersonic exit velocity . Because the ...
... nozzle efficiency , which is normally very close to 1 . [ 6.25 ] The nozzle performance equations work just as well for rocket engines except that rocket nozzles always expand the flow to some supersonic exit velocity . Because the ...
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