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Improved computer programs for calculating potential flow in propulsion system inletsComputer programs to calculate the incompressible potential flow corrected for compressibility in axisymmetric inlets at arbitrary operating conditions are presented. Included are a statement of the problem to be solved, a description of each of the programs and sufficient documentation, including a test case, to enable a user to run the programs.
Document ID
19770026220
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stockman, N. O. (NASA Lewis Research Center Cleveland, OH, United States)
Farrell, C. A., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-9285
NASA-TM-73728
Report Number: E-9285
Report Number: NASA-TM-73728
Accession Number
77N33164
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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