Perspective of Combustion Modeling for Gas Turbine Combustors-Reference-Cited by-同舟云学术

Perspective of Combustion Modeling for Gas Turbine Combustors

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Mongia Hukam¹

Affiliation:

1. GE Aircraft Engines

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-156

Reference48 articles.

1. Mongia, H. C., and Smith, K. F., 1978, "An empirical/analytical design methodology for gas turbine combustor",AIAA Paper78-998.

2. Hsiao, G., and Mongia, H., 2003, "Swirl cup modeling, Part 3: Grid independent solution with different turbulencemodels,"AIAA Paper2003-1349.

3. Mongia, H. C., Reynolds, R. S., Coleman, E., and Bruce, T. W., 1979, "Combustor Design Criteria Validation Volume I -Element tests and model validation", USARTL-TR-78-55A(AD-AO-67657).

4. Giridharan, M., Mongia, H., and Singh, G., 2003, "Scaling of dilution hole inlet conditions for gas turbine combustorCFD models,"AIAAPaper2003-1203.

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