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An experimental study of the pressure and heat-transfer distribution on a 70 deg sweep slab delta wing in hypersonic flowPressure, heat transfer & force distribution on slab delta wing in air and helium hypersonic flow
Document ID
19640009807
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Bertram, M. H. (NASA Langley Research Center Hampton, VA, United States)
Everhart, P. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TR-R-153
Report Number: NASA-TR-R-153
Accession Number
64N19721
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
AERODYNAMIC HEAT TRANSFER
PRESSURE DISTRIBUTION
HYPERSONIC FLOW

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