NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Calculation of two-dimensional inlet flow fields in a supersonic free stream: Program documentation and test casesThe use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic free stream and a nonorthogonal mesh-generation code are illustrated by specific examples. Input, output, and program operation and use are given and explained for the case of supercritical inlet operation at a subdesign Mach number (M Mach free stream = 2.09) for an isentropic-compression, drooped-cowl inlet. Source listings of the computer codes are also provided.
Document ID
19800008769
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biringen, S. H. (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
March 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3221
NEAR-TR-195
Report Number: NASA-CR-3221
Report Number: NEAR-TR-195
Accession Number
80N17029
Funding Number(s)
CONTRACT_GRANT: NAS1-15305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available