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Design of two-dimensional sharp-edged-throat supersonic nozzle with boundary-layer correctionComputer program accounts for effective nozzle geometry changes due to boundary layer displacement thickness. Program input and output are discussed.
Document ID
19720000070
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Goldman, L. J.
Vanco, M. R.
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11636
Report Number: LEW-11636
Accession Number
72B10070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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