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Shock tube instrumentation techniques for study of hypervelocity entry problems.Shock tube instrumentation to study convective and radiative heat transfer of hot gases simulating hypervelocity reentry
Document ID
19650052518
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gruszczynski, J. S.
Rogers, D. A.
Date Acquired
August 2, 2013
Publication Date
August 1, 1965
Subject Category
Facilities, Research, And Support
Accession Number
65A35222
Funding Number(s)
CONTRACT_GRANT: JPL-950297
Distribution Limits
Public
Copyright
Other
Keywords
CONVECTIVE HEAT TRANSFER
SHOCK MEASURING APPARATUS
HYPERSONIC HEAT TRANSFER
REENTRY PHYSICS

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