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http://dx.doi.org/10.5139/JKSAS.2016.44.2.99

Test Research Using an IR Thermography Technique in a Supersonic Wind Tunnel  

Kim, Ikhyun (Korea Advanced Institute of Science and Technology)
Lee, Jaeho (Agency for Defense Development)
Park, Gisu (Korea Advanced Institute of Science and Technology)
Byun, Yunghwan (Konkuk University)
Lee, Jongkook (Agency for Defense Development)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.44, no.2, 2016 , pp. 99-107 More about this Journal
Abstract
Test research on Infra-Red Thermography(IRT) technique in a supersonic wind tunnel has been conducted. Inadvertent technical difficulties and their solutions associated with the technique in running of the facility were examined. Two flow conditions at Mach number of 3 and 4 were considered. A double compression ramp model, that replicates realistic high-speed vehicle configuration, was used as test model. The present IR data were compared with shadowgraph visualization images and laminar computational fluid dynamics(CFD) results. It has been shown that the IRT technique can be used in quantifying various fluid dynamic features such as flow transition, separation and three-dimensional phenomena around the double compression ramp model.
Keywords
Infra-Red Thermography; Separation Shock; Reattachment Shock; Flow Transition; Compression Ramp;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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