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Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory

Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory - - Washington, D.C. National Aeronautics & Space Administration 1978 - 57 p. - NASA TP 1345 : 1978 .

ISBN:

Subjects--Topical Terms:

Actuator disk theory, Flutter, Supersonic speeds, Compressors

Universal Decimal Class. No.: LNASA TP 1345 : 1978

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