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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