LATERAL JET INJECTION INTO ISOTHERMAL COMBUSTOR FLOWFIELDS
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/10.1080/00986448708911910
Reference21 articles.
1. Gas turbine engine pollution
2. Novick , A.S. Arvin , J.R. , and Ouinn , R.E. “ Development of a Gas Turbine Combustor Dilution Zone Design Analysis ”, AIAA Paper No, 79–1194, AIAA/SAE/ASME 15th Joint Propulsion Conference, Las Vegas, Nevada, June 8–10 , 1979 .
3. Mellor , A.M. “ Semi-Empirical Correlations for Gas Turbine Emissions, Ignition and Flame Stabilization ”, AGARD Conference Reprint No. 275, Combustion Modeling, AGARD , pp. p24.2–24.13 p, 1979 .
4. Sturgess , G. “ Gas Turbine Combustor Design Challenges for 1980's ”, AIAA Paper No. 80–1285, AIAA/SAE/ASME 16th Joint Propulsion Conference , Hartford , Conneticut , June 30-July 2 , 1980 .
5. Holdeman , J.D. “ Prespectives on the Mixing of a Row of Jets with a Confined Crossflow ”, AIAA paper No. 83–1200, AIAA/SAE/ASME 19th Joint Propulsion Conference , Seattle , Washington , June 27–29 , 1983 .
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