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Stagnation point flow with radiationCoupling between inviscid and viscid flows in hypersonic stagnation region investigated at high flight velocities with significant radiative heat transfer
Document ID
19660007695
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chisnell, R. F. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Hoshizaki, H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Lasher, L. E. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
LMSC-4-43-65-4
NASA-CR-70171
Report Number: LMSC-4-43-65-4
Report Number: NASA-CR-70171
Accession Number
66N16984
Funding Number(s)
CONTRACT_GRANT: NAS7-295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
STAGNATION REGION
INVISCID FLOW
VISCOUS FLOW
RADIATIVE HEAT TRANSFER

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