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Experimental assessment of the effect of large amounts of argon in a planetary atmosphere on stagnation-point convective heating.Atmospheric argon effect on hypersonic stagnation point convective heat transfer, using arc-heated shock tube simulating flight velocities up to 34,000 fps
Document ID
19660038601
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Babineaux, T. L.
Horton, T. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 66-29
Report Number: AIAA PAPER 66-29
Accession Number
66A17891
Distribution Limits
Public
Copyright
Other
Keywords
ARGON
ATMOSPHERIC COMPOSITION
SHOCK TUNNEL
STAGNATION POINT
CONVECTIVE HEAT TRANSFER
HYPERSONIC FLOW

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