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Applied high-speed imaging for the icing research program at NASA Lewis Research CenterThe Icing Research Tunnel at NASA Lewis Research Center provides scientists a scaled, controlled environment to simulate natural icing events. The closed-loop, low speed, refrigerated wind tunnel offers the experimental capability to test for icing certification requirements, analytical model validation and calibration techniques, cloud physics instrumentation refinement, advanced ice protection systems, and rotorcraft icing methodology development. The test procedures for these objectives all require a high degree of visual documentation, both in real-time data acquisition and post-test image processing. Information is provided to scientific, technical, and industrial imaging specialists as well as to research personnel about the high-speed and conventional imaging systems will be on the recent ice protection technology program. Various imaging examples for some of the tests are presented. Additional imaging examples are available from the NASA Lewis Research Center's Photographic and Printing Branch.
Document ID
19930049172
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Slater, Howard
(NASA Lewis Research Center Cleveland, OH, United States)
Owens, Jay
(Cortez III Services Corp. Brook Park, OH, United States)
Shin, Jaiwon
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Ultrahigh- and high-speed photography, videography, and photonics '91; Proceedings of the Meeting, San Diego, CA, July 24-26, 1991 (A93-33165 12-35)
Publisher: Society of Photo-Optical Instrumentation Engineers
Subject Category
Instrumentation And Photography
Accession Number
93A33169
Funding Number(s)
CONTRACT_GRANT: NAS3-24816
Distribution Limits
Public
Copyright
Other

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