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Unstady flow in a supersonic cascade with two in-passage shocks

Unstady flow in a supersonic cascade with two in-passage shocks - - Washington, D.C. National Aeronautics and Space Adminstration 1985 - 89 p. - NASA CR 3925 : 1985 .

ISBN:

Subjects--Topical Terms:

Flutter, Compressor, Supersonic flow, Shock waves

Universal Decimal Class. No.: LNASA CR 3925 : 1985

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