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Inlet-air distortion effects on stall, surge, and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes
Author:
Harry, David P , III
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E54K26
Link:
https://digital.library.unt.edu/ark:/67531/metadc61122/
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