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 125
... compressor the flow travels par- allel to the axis of rotation ( i.e. , in the axial direction ) . In a centrifugal ... compressor increases the airflow pressure by a factor of 4. In the cen- trifugal compressor , the additional pressure ...
... compressor the flow travels par- allel to the axis of rotation ( i.e. , in the axial direction ) . In a centrifugal ... compressor increases the airflow pressure by a factor of 4. In the cen- trifugal compressor , the additional pressure ...
Page 126
... compressor becomes a design constraint ( i.e. , a fac- tor limiting the engine performance ) due to temperature limits on the compres- sor material , especially the last compressor stage . 6.3.3 Burner or Combustor The burner is where ...
... compressor becomes a design constraint ( i.e. , a fac- tor limiting the engine performance ) due to temperature limits on the compres- sor material , especially the last compressor stage . 6.3.3 Burner or Combustor The burner is where ...
Page 129
... compressor stage . A single turbine stage can be used to drive multiple compressor stages . To keep flow from leak- ing around the edges of the turbine blades , because of the higher pressure gradi- ent , the tips of the turbine blades ...
... compressor stage . A single turbine stage can be used to drive multiple compressor stages . To keep flow from leak- ing around the edges of the turbine blades , because of the higher pressure gradi- ent , the tips of the turbine blades ...
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