Publication Date:
2006-07-16
Description:
A technology assessment of turbomachinery is presented. The design of the fan, compressor, and turbine components for future advanced aircraft engines is discussed. Basic flow characteristics in compressors and turbines and the heat transfer phenomena in cooled turbines are also discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
Aeropropulsion 1979; p 231-272
Format:
text
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