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Raman scattering applied to gas mixing in the successive channel flow of two gasesThe Raman scattering technique has been applied to investigate the effects of fluid undercutting in a simulation of the fluid-piston concept for wind-tunnel design. Measurements of the structure of the driver-driven gas interface and of the effect of undercutting on test duration were performed. Tests were conducted over a Froude number range of 0.0021 to 0.526 at driver-to-driven gas density ratios of 1.103 and 1.573. The effects of inlet design, test-channel inclination angle, and pretest pressurization were also examined. The results are compared with shadowgraph and pressure measurements to illustrate the characteristics of the Raman technique and to explain the discrepancy between the shadowgraph and pressure results.
Document ID
19740043749
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hillard, M. E., Jr.
Guy, R. W.
Emory, M. L.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: ICIASF ''73; International Congress on Instrumentation in Aerospace Simulation Facilities
Location: Pasadena, CA
Start Date: September 10, 1973
End Date: September 12, 1973
Accession Number
74A26499
Distribution Limits
Public
Copyright
Other

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