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Performance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region

Performance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region - - Washington,D.C. National Aeronautics & Space Administration 1978 - 82 p. - NASA TP 1293 : 1978 .

ISBN:

Subjects--Topical Terms:

Turbomachinery, Transonic compressors, Inlet radial distortion

Universal Decimal Class. No.: LNASA TP 1293 : 1978

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