Publication Date:
2019-07-13
Description:
A 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.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-102422
,
E-5063
,
NAS 1.15:102422
,
AVSCOM-TR-89-C-013
,
AD-A233938
,
International Symposium on Combustion; Jul 22, 1990 - Jul 27, 1990; Orleans; France
Format:
application/pdf
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