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Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test caseThe source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.
Document ID
19810017541
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biringen, S. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Mcmillan, O. J. (Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3414
NEAR-TR-233
Report Number: NASA-CR-3414
Report Number: NEAR-TR-233
Accession Number
81N26077
Funding Number(s)
CONTRACT_GRANT: NAS1-15951
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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