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Computer program for design of two-dimensional sharp-edged-throat supersonic nozzle with boundary layer correctionFORTRAN 4 computer program for design of sharp-edged-throat supersonic nozzles with boundary layer correction
Document ID
19710023317
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goldman, L. J. (NASA Lewis Research Center Cleveland, OH, United States)
Vanco, M. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
E-6261
NASA-TM-X-2343
Report Number: E-6261
Report Number: NASA-TM-X-2343
Accession Number
71N32793
Funding Number(s)
CONTRACT_GRANT: 120-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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