Experimental study of novel passive control methods to improve combustor exit temperature uniformity
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s00231-014-1357-6.pdf
Reference20 articles.
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2. Barringer MD, Richard OT, Walter JP, Stitzel SM, Thole KA (2002) Flow field simulations of a gas turbine combustor. J Turbomach 124:508–516
3. Chen Y, Aung K, Glezer A, Jagoda J (1999) Enhanced mixing in a simulated combustor using synthetic jet actuators. 37th AIAA aerospace sciences meeting and exhibit, Reno
4. Doerr T, Blomeyer M, Hennecke DK (1997) Optimization of multiple jets mixing with a confined crossflow. J Eng Gas Turbines Power 119(2):315–321
5. Gulati A, Tolpadi A, VanDeusen G (1995) Effect of dilution air on the scalar flowfield at combustor sector exit. J Propul Power 11:1162–1169
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