This paper provides an overview of recent wind tunnel tests performed at the NASA Langley Research Center where the Background-Oriented Schlieren (BOS) technique was used to provide information pertaining to flow-field density disturbances. The facilities in which the BOS technique was applied included the National Transonic Facility (NTF), Transonic Dynamics Tunnel (TDT), 31-Inch Mach 10 Air Tunnel, 15-Inch Mach 6 High-Temperature Air Tunnel, Rotor Test Cell at the 14 by 22 Subsonic Tunnel, and a 13-Inch Low-Speed Tunnel.
Development of Background-Oriented Schlieren for NASA Langley Research Center Ground Test Facilities
AIAA Science and Technology Forum and Exposition ; 2015 ; Kissimmee, FL, United States
2015-01-05
Conference paper
No indication
English
British Library Conference Proceedings | 2015
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