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Imaging Supersonic Aircraft Shock WavesA schlieren imaging system that uses the sun as a light source was developed it) obtain direct flow-field images of shock waves of aircraft in flight. This system was used to study how shock waves evolve to form sonic booms. The image quality obtained was limited by several optical and mechanical factors. Converting the photographs to digital images and applying digital image-processing techniques greatly improved the final quality of the images and more clearly showed the shock structures.
Document ID
19990084093
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Weinstein, Leonard M.
(NASA Langley Research Center Hampton, VA United States)
Stacy, Kathryn
(NASA Langley Research Center Hampton, VA United States)
Vieira, Gerald J.
(NASA Wallops Flight Facility Wallops Island, VA United States)
Haering, Edward A., Jr.
(NASA Dryden Flight Research Center Edwards, CA United States)
Bowers, Albion H.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1997
Publication Information
Publication: Journal of Flow Visualization and Image Processing
Publisher: Begell House, Inc.
Volume: 4
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Other

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