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Computer programs for calculating potential flow in propulsion system inletsCalculational procedure evolved in process of designing inlets. Douglas axisymmetric potential flow program called EOD calculates incompressible potential flow about arbitrary bodies. Program SCIRCL generates input for EOD from inlet components. Program COMBYN takes basic solutions output by EOD and combines them into solutions of interest and applied compressibility correction.
Document ID
19750000018
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stockman, N. O.
Button, S. L.
Date Acquired
August 8, 2013
Publication Date
April 1, 1975
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-12152
Report Number: LEW-12152
Accession Number
75B10018
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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