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Modification of axial compressor streamline program for analysis of engine test dataAn existing axial compressor streamline analysis computer program to allow input of measured radial pressure and temperature profiles obtained from engine or cascade data is described. The proposed modifications increase the input flexibility and are accomplished without changing the computer program's input format.
Document ID
19800005795
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Williams, J. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-79312
E-268
Report Number: NASA-TM-79312
Report Number: E-268
Accession Number
80N14051
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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