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
Effect of hinge-line bleed on heat transfer and pressure distribution over a wedge-flap combination at Mach 10.4Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface at hypersonic speeds
Document ID
19680020483
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dearing, J. D. (NASA Langley Research Center Hampton, VA, United States)
Hamilton, H. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4686
Report Number: NASA-TN-D-4686
Accession Number
68N29955
Funding Number(s)
CONTRACT_GRANT: 129-01-07-08-23
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