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Hypersonic boundary-layer transition on ablating and nonablating conesAblation effects on transition Reynolds number of hypersonic boundary layer on slender cones
Document ID
19700036829
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fischer, M. C.
Date Acquired
August 5, 2013
Publication Date
October 1, 1969
Subject Category
Fluid Mechanics
Accession Number
70A12945
Distribution Limits
Public
Copyright
Other

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