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
A study of pressure and heat transfer over an 80 deg sweep slab delta wing in hypersonic flowPressure and heat transfer over 80-degree sweep slab delta wing in hypersonic flow - wind tunnel test
Document ID
19650009678
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dunavant, J. C. (NASA Langley Research Center Hampton, VA, United States)
Whitehead, A. H., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2708
Report Number: NASA-TN-D-2708
Accession Number
65N19279
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
SWEPT WING
DELTA WING
HEAT TRANSFER

Related Records

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