MODELING OF LATERAL JETS INJECTED INTO SWIRLING CROSSFLOW
Author:
Affiliation:
1. a Department of Mechanical and Industrial Engineering , Clarkson University , Potsdam , New York , 13676
Publisher
Informa UK Limited
Subject
General Chemical Engineering,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/00986448908940196
Reference21 articles.
1. Novic , A.S. , Arvin , J.R. , and Quinn , R.E. “ Development of a Gas Turbine Combustor Dilution Zone Design Analysis, ” AIAA/SAE/ASME 15th Joint Propulsion Conference , Las Vegas , Nevada , June , 1979 8 - 10 .
2. Sturgess , G. “ Gas Turbine Combustor Design Challenges for 1980's, ” AIAA Paper No. 80–1285 , AIAA/SAE/ASME 16th Joint Conference, Hartford , Connecticut , June 30- July 2, 1980 .
3. Mixing of a Row of Jets with a Confined Crossflow
4. Mularz , E.J. (ed.), “ Combustion Fundamentals Research Conference, ” held at NASA Lewis Research Center, Cleveland , Ohio , October 21 – 22 , 1982 .
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1. Mixing of multiple jets with a confined subsonic crossflow;Progress in Energy and Combustion Science;1993-01
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