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Principles and application of shock-tubes and shock tunnelsThe principles, theoretical flow equations, calculation techniques, limitations and practical performance characteristics of basic and high performance shock tubes and shock tunnels are presented. Selected operating curves are included.
Document ID
19740009843
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ried, R. C. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Clauss, H. G., Jr. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
October 22, 1963
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-69941
WORKING-PAPER-10014
Report Number: NASA-TM-X-69941
Report Number: WORKING-PAPER-10014
Accession Number
74N17956
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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