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Non-Intrusive Measurement Techniques for Flow Characterization of Hypersonic Wind TunnelsThis manuscript describes the wide variety of optical measurement techniques for characterizing the flow in hypersonic wind tunnels. The introduction briefly describes different types of hypersonic wind tunnels, why they are used, and typical freestream conditions including fluctuating quantities. Description of these conditions defines the challenge for measurement techniques which have varying degrees of accuracy and precision, and work only in certain temperature, density and/or speed regimes. The rest of the manuscript is broken up into sections, by measurement technique. Each technique is described and then several examples are provided. The concluding chapter compares and contrasts different aspects of the measurement techniques including accuracy, precision, spatial resolution and temporal resolution.
Document ID
20190029251
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Danehy, P. M.
(NASA Langley Research Center Hampton, VA, United States)
Weisberger, J.
(NASA Langley Research Center Hampton, VA, United States)
Johansen, C.
(University of Calgary Calgary, Alberta, Canada)
Reese, D.
(National Inst. of Aerospace Hampton, VA, United States)
Fahringer, T.
(National Inst. of Aerospace Hampton, VA, United States)
Parziale, N. J.
(Stevens Institute of Technology Hoboken, NJ, United States)
Dedic, C.
(Virginia Univ. Charlottesville, VA, United States)
Estevadeordal, J.
(North Dakota State Univ. Fargo, ND, United States)
Cruden, B. A.
(Analytical Mechanics Associates, Inc. Sunnyvale, CA, United States)
Date Acquired
August 21, 2019
Publication Date
December 3, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-31725
Meeting Information
Meeting: STO-VKI-LS on "Flow Characterization and Modeling of Hypersonic Wind Tunnels"
Location: Sint-Genesius-Rode
Country: Belgium
Start Date: December 3, 2018
End Date: December 5, 2018
Sponsors: Von Karman Inst. for Fluid Dynamics
Distribution Limits
Public
Copyright
Public Use Permitted.
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