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A planar reacting shear layer system for the study of fluid dynamics-combustion interactionA versatile planar reacting shear layer facility is constructed at NASA-Lewis. The research objectives, as well as design, instrumentations and the operational procedures developed for the system are described. The fundamental governing equations and the type of quantitative information that are needed from experiments are described. Additionally, a review of earlier work is presented. Whenever appropriate, comparisons are made with similar systems in other facilities and the main differences are described. Finally, the nonintrusive measurement techniques (PLIF, PMS, LDV, and Schlieren photography) and the type of experiments that are planned are described.
Document ID
19900004077
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marek, C. J. (NASA Lewis Research Center Cleveland, OH., United States)
Chang, C. T. (NASA Lewis Research Center Cleveland, OH., United States)
Ghorashi, B. (Cleveland State Univ. OH., United States)
Wey, C. C. (Cleveland State Univ. OH., United States)
Wey, C. (Sverdrup Technology, Inc., Cleveland OH., United States)
Mularz, E. J. (Army Aviation Research and Development Command Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-102422
AVSCOM-TR-89-C-013
E-5063
NAS 1.15:102422
AD-A233938
Meeting Information
Meeting: International Symposium on Combustion
Location: Orleans
Country: France
Start Date: July 22, 1990
End Date: July 27, 1990
Sponsors: Orleans Univ.
Accession Number
90N13393
Funding Number(s)
PROJECT: DA PROJ. 1L1-61102-AH-45
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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