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Static-pressure contours in the blade passage at the tip of several high Mach number rotorsStatic pressure contours of turbine rotor blade tips at high Mach numbers
Document ID
19710007772
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bailey, E. E. (NASA Lewis Research Center Cleveland, OH, United States)
Miller, G. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2170
E-5875
Report Number: NASA-TM-X-2170
Report Number: E-5875
Accession Number
71N17247
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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