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Free stream turbulence and density ratio effects on the interaction region of a jet in a cross flowJets of low temperature air are introduced into the aft sections of gas turbine combustors for the purpose of cooling the high temperature gases and quenching the combustion reactions. Research studies, motivated by this complex flow field, have been executed by introducing a heated jet into the cross stream of a wind tunnel. The investigation by Kamotani and Greber stands as a prime example of such investigations and it serves as the principal reference for the present study. The low disturbance level of the cross stream, in their study and in similar research investigations, is compatible with an interest in identifying the basic features of this flow field. The influence of the prototypes' strongly disturbed cross flow is not, however, made apparent in these prior investigations.
Document ID
19840012478
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wark, C. E.
(Michigan State Univ. East Lansing, MI, United States)
Foss, J. F.
(Michigan State Univ. East Lansing, MI, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
84N20546
Funding Number(s)
CONTRACT_GRANT: NAG3-245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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