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Numerical solution of the hypersonic viscous shock-layer equationsViscous shock layer equations of laminar hypersonic flow past blunt body at moderate to high Reynolds numbers
Document ID
19700053836
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Davis, R. T.
Date Acquired
August 5, 2013
Publication Date
May 1, 1970
Subject Category
Aerodynamics
Accession Number
70A29952
Funding Number(s)
CONTRACT_GRANT: NGR-47-004-006
Distribution Limits
Public
Copyright
Other

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