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AN INVESTIGATION OF FLOW VISUALIZATION TECHNIQUES IN HELIUM AT MACH NUMBERS OF 15 AND 20Flow visualization techniques in helium at mach 15 & 20 - surface streamlines, attached and separated afterbody flow & stagnation points
Document ID
19630004712
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Duller, C. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1769
Report Number: NASA-TN-D-1769
Accession Number
63N14588
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STAGNATION POINT
HYPERSONIC FLOW
FLOW VISUALIZATION
FLOW SEPARATION
HELIUM

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