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 120
... inlet velocity because the propeller accelerates the air . In reality , the thrust depends on the inlet velocity , but we assume that for our purposes the propeller is moving much faster ( meas- ured in revolutions per minute ) than our ...
... inlet velocity because the propeller accelerates the air . In reality , the thrust depends on the inlet velocity , but we assume that for our purposes the propeller is moving much faster ( meas- ured in revolutions per minute ) than our ...
Page 123
... Inlet or Intake The freestream air enters the gas turbine engine at the inlet , also referred to as the intake . While the inlet does no work on the flow , there are important engi- neering design features to this component . Inlets ...
... Inlet or Intake The freestream air enters the gas turbine engine at the inlet , also referred to as the intake . While the inlet does no work on the flow , there are important engi- neering design features to this component . Inlets ...
Page 124
... inlet must slow the flow down to subsonic speeds before the air reaches the compres- sor . Some supersonic inlets ... inlet geometry having a rectangular cross section ( Figure 6.4 , bottom left ) . This kind of inlet is seen on the F ...
... inlet must slow the flow down to subsonic speeds before the air reaches the compres- sor . Some supersonic inlets ... inlet geometry having a rectangular cross section ( Figure 6.4 , bottom left ) . This kind of inlet is seen on the F ...
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