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Problems and solutions for transition detection in cryogenic wind tunnels by infrared imagingThe authors analyzed the problems associated with the detection of boundary-layer transition to turbulence by using the IR imaging techique in cryogenic wind-tunnel testing. It is shown that testing at low temperatures forces this implementation to run against the physical laws of diminishing returns. The most difficult obstacle resulted from the considerable decrease in the overall level of IR radiation and the parallel shift of the bulk of the radiated energy to longer wavelengths, beyond 30 microns at 100 K. Some measures to alleviate the problem are described. The thermal signature of transition can be enhanced by allowing the flow in the wind tunnel to heat incrementally, thus inducing a transient heat transfer to the model. As a result, the model area under the turbulent regime is revealed by its higher heating rate compared to the laminar regime.
Document ID
19920071695
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gartenberg, Ehud
(Old Dominion University Norfolk, VA, United States)
Wright, Robert E., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Research And Support Facilities (Air)
Meeting Information
Meeting: ICIASF ''91 - International Congress on Instrumentation in Aerospace Simulation Facilities
Location: Rockville, MD
Country: United States
Start Date: October 27, 1991
End Date: October 31, 1991
Accession Number
92A54319
Funding Number(s)
CONTRACT_GRANT: NAS1-18584
Distribution Limits
Public
Copyright
Other

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