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Transition and turbulence measurements in hypersonic flowsThis paper reviews techniques for transitional- and turbulent-flow measurements and describes current research in support of turbulence modeling. Special attention is given to the potential of applying hot wire and laser velocimeter to measuring turbulent fluctuations in hypersonic flow fields. The results of recent experiments conducted in two hypersonic wind tunnels are presented and compared with previous hot-wire turbulence measurements.
Document ID
19910029834
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Owen, F. K.
(Complere, Inc. Palo Alto, CA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-5231
Accession Number
91A14457
Funding Number(s)
CONTRACT_GRANT: NAS2-12853
CONTRACT_GRANT: F33615-88-C-3014
Distribution Limits
Public
Copyright
Other

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