Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers I : rotor design and over-all performance at tip speeds from 60 to 100 percent of design

Serovy, George K Robbins, William H Glaser, Frederick W
naca-rm-e53i11
December 07, 1953


No Abstract Available

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