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Low-density, leading-edge bluntness, and ablation effects on wedge-induced laminar boundary layer separation at moderate enthalpies in hypersonic flowLow density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer separation at moderate enthalpies in hypersonic flow
Document ID
19680026986
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Anders, J. B. (NASA Langley Research Center Hampton, VA, United States)
Edwards, C. L. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-4829
Accession Number
68N36458
Funding Number(s)
CONTRACT_GRANT: 129-01-03-15-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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