NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Hypersonic laminar boundary layers around slender bodiesCompressible laminar boundary layer equations considered for hypersonic flow around slender bodies
Document ID
19680019701
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jeng, D. R.
(Alabama Univ. Huntsville, AL, United States)
Yalamanchili, R. V. S.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-95768
UARI-55
Accession Number
68N29173
Funding Number(s)
CONTRACT_GRANT: NSG-381
CONTRACT_GRANT: NGR-01-002-001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available