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 ...
... 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 ...
Page 132
... nozzle efficiency , which is normally very close to 1 . nn [ 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 ...
... nozzle efficiency , which is normally very close to 1 . nn [ 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 ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing