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
Effects of leading-edge bluntness on pressure and heat-transfer measurements over a flat plate at a mach number of 20Effects of leading edge bluntness on pressure and heat transfer at hypersonic speed
Document ID
19650025456
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Harvey, W. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-2846
Report Number: NASA-TN-D-2846
Accession Number
65N35057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HEAT TRANSFER
LEADING EDGE
PRESSURE EFFECT
HYPERSONIC SPEED
AEROTHERMODYNAMICS
BLUNT BODY

Related Records

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