Experimental and Numerical Investigations on Liner Cooling Characteristics of a Trapped Vortex Combustor-Reference-Cited by-同舟云学术

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Experimental and Numerical Investigations on Liner Cooling Characteristics of a Trapped Vortex Combustor

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Jingyu Zhang¹,Xiaomin He¹,Yi Jin¹,Lu Wang¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3767

Reference15 articles.

1. Hsu K Y, Goss L P. Trump D D, Performance of a trapped-vortexcombustor[R].AIAA95-0810.

2. Characteristics of a Trapped-Vortex Combustor

3. Burrus D L, Johnson A W, Mroquemore M, Shouse D T. Performance assessment of a prototype trapped vortex combustor concept for gas turbine application[R].2001-GT-0087.

4. Hendricks R C. Experimental and computational study of trapped vortex combuster sector rig with tri-passdiffuser [R].NASA/TM-2004-212507.

5. HE Xiaomin, XU Jinsheng, SU Junqing. Experi-mental research of the performance of the trapped-vortex combustor[J].Journal of Aero-space Power,2009,24(2):318-323.

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