Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници 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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Страница 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 ...
Страница 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 ...
Страница 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 ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
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