NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Computer programs for calculating potential flow in propulsion system inletsIn the course of designing inlets, particularly for VTOL and STOL propulsion systems, a calculational procedure utilizing three computer programs evolved. The chief program is the Douglas axisymmetric potential flow program called EOD which calculates the incompressible potential flow about arbitrary axisymmetric bodies. The other two programs, original with Lewis, are called SCIRCL AND COMBYN. Program SCIRCL generates input for EOD from various specified analytic shapes for the inlet components. Program COMBYN takes basic solutions output by EOD and combines them into solutions of interest, and applies a compressibility correction.
Document ID
19730020450
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stockman, N. O.
(NASA Lewis Research Center Cleveland, OH, United States)
Button, S. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-68278
Report Number: NASA-TM-X-68278
Accession Number
73N29182
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available