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

Contributor(s): Language: English Series: NASA TP 1345 : 1978Publication details: Washington, D.C. ; National Aeronautics & Space Administration ; 1978Edition: Description: 57 p; ISBN: Subject(s): | Actuator disk theory, Flutter, Supersonic speeds, CompressorsOnline resources: Click here to access online
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Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA TP 1345 : 1978 Not for loan A39171
Total holds: 0

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