Numerical simulation of cavity flow structure in an axisymmetric trapped vortex combustor-Reference-Cited by-同舟云学术

Numerical simulation of cavity flow structure in an axisymmetric trapped vortex combustor

Published:2012-09 Issue:1 Volume:21 Page:16-23
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ezhil Kumar P.K.,Mishra D.P.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Numerical modeling of an axisymmetric trapped vortex combustor;Ezhil Kumar;International Journal of Turbo and Jet Engines,2011

2. P.K. Ezhil Kumar, D.P. Mishra, Effect of momentum flux ratio on non-reacting flow structure in an axisymmetric trapped vortex combustor, in: 10th Asian Symposium on Visualization, 2010, pp. 477–486.

3. Characteristics of a trapped vortex combustor;Hsu;Journal of Propulsion and Power,1998

4. K.Y. Hsu, L.P. Goss, D.D. Trump, Performance of a trapped vortex combustor, AIAA paper 95-0810, January 1995.

5. Study on trapped-vortex combustor – effect of injection on flow dynamics;Katta;Journal of Propulsion and Power,1998

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