DESIGN CONSIDERATIONS IN ADVANCED GAS TURBINE COMBUSTION CHAMBERS-Reference-Cited by-同舟云学术

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DESIGN CONSIDERATIONS IN ADVANCED GAS TURBINE COMBUSTION CHAMBERS

Published:1968 Issue: Volume: Page:3-19
ISSN:
Container-title:Combustion in Advanced Gas Turbine Systems
language:
Short-container-title:

Author:

LEFEBVRE ARTHUR H.

Publisher

Elsevier

Reference5 articles.

1. High Performance Turbine Engines

2. JEFFS, R. A. Eighth Symposium (International) on Combustion, p. 1014. Williams & Wilkins, 1962.

3. LEFEBVRE, A. H. Tenth Symposium (International) on Combustion, p. 1129. The Combustion Institute, 1965.

4. LEFEBVRE, A. H. and MILLER, D. The Development of an Air-Blast Atomizer for Gas Turbine Application, College of Aeronautics Report, Aero. No. 193, 1966.

5. LEFEBVRE, A. H. British Patent No. 1,031,184.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Soot Studies in Gas Turbine Combustors and other Turbulent Spray Flames;Particulate Carbon;1981

2. Computer modeling of turbulent reacting flows in practical combustion chamber design;17th Aerospace Sciences Meeting;1979-01-15

3. Second Paper: Experiments on a Transpiration Cooled Combustion Chamber;Proceedings of the Institution of Mechanical Engineers;1973-06

4. Second Paper: Experiments on a Transpiration Cooled Combustion Chamber;Proceedings of the Institution of Mechanical Engineers;1973-06

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