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Experimentally measured effects of the wall boundary layer on shock-tube performanceNitrogen driven gas wall boundary layer effect and hydrogen driver gas thermodynamic effect on shock speed and test time in tube
Document ID
19650009668
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Livingston, F. R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
JPL-TR-32-714
NASA-CR-57266
Report Number: JPL-TR-32-714
Report Number: NASA-CR-57266
Accession Number
65N19269
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMODYNAMICS
NITROGEN
HYDROGEN
TEST TIME
SHOCK TUNNEL

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