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Potential flows in propulsion system inletsCollection of computer programs used to calculate compressible potential flow in arbitrary axisymmetric inlet at any combination of operating conditions of inlet mass-flow rate, free stream velocity, and incident angle proves useful in development of wide variety of propulsion system inlet designs.
Document ID
19780000553
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Farrell, C. A., Jr.
Stockman, N. O.
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13010
Report Number: LEW-13010
ISSN: 0145-319X
Accession Number
78B10553
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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