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Background-Oriented Schlieren for Large-Scale and High-Speed Aerodynamic PhenomenaVisualization of the flow field around a generic re-entry capsule in subsonic flow and shock wave visualization with cylindrical explosives have been conducted to demonstrate sensitivity and applicability of background-oriented schlieren (BOS) for field experiments. The wind tunnel experiment suggests that BOS with a fine-pixel imaging device has a density change detection sensitivity on the order of 10(sup -5) in subsonic flow. In a laboratory setup, the structure of the shock waves generated by explosives have been successfully reconstructed by a computed tomography method combined with BOS.
Document ID
20160005917
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Mizukaki, Toshiharu
(Tokai Univ. Kanagawa, Japan)
Borg, Stephen
(NASA Langley Research Center Hampton, VA, United States)
Danehy, Paul M.
(NASA Langley Research Center Hampton, VA, United States)
Murman, Scott M.
(NASA Ames Research Center Moffett Field, CA, United States)
Matsumura, Tomoharu
(National Inst. of Advanced Industrial Science and Technology Tsukuba, Japan)
Wakabayashi, Kunihiko
(National Inst. of Advanced Industrial Science and Technology Tsukuba, Japan)
Nakayama, Yoshio
(National Inst. of Advanced Industrial Science and Technology Tsukuba, Japan)
Date Acquired
May 6, 2016
Publication Date
January 5, 2015
Subject Category
Instrumentation And Photography
Report/Patent Number
NF1676L-20452
Report Number: NF1676L-20452
Meeting Information
Meeting: AIAA SciTech 2015
Location: Orlando, FL
Country: United States
Start Date: January 5, 2015
End Date: January 8, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 122711.03.09.07.01.17
Distribution Limits
Public
Copyright
Public Use Permitted.
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