Gas turbine combustor liner wall temperature calculation methodology-Reference-Cited by-同舟云学术

Gas turbine combustor liner wall temperature calculation methodology

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
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Author:

Mongia Hukam¹

Affiliation:

1. GE Aircraft Engines, Cincinnati, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3267

Reference42 articles.

1. Rizk, N. K., etal, 1988, "High Density Fuel Effects", AFWAL-TR-88-2046.

2. Bruce, T. W., Davis, F. G., Kuhn, T. E., and Mongia, H. C., 1977, "Pollution Reduction Technology Program Small Jet Engines Phase I Final Report", NASACR-135214. 3. 1CAOEngine Exhaust Emissions database

3. Burrus, D. L. "Energy Efficient Engine Combustion System Component Technology Development Report," NASA Contract NAS3-20643 Report R82AEB401.

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