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General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines
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English
Abstract
This paper reviews those requirements that are common in the design of all gas turbines combustion equipment. Where necessary, a distinction is made between the demands of industrial and aircraft chambers. The problem of designing equipment for long life and low pressure loss, in a size compatible with the overall engine, is discussed in detail, and the application of combustor characteristics and design factors to the demands of new aircraft and industrial turbines are anticipated.
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Citation
Clarke, J. and Jackson, S., "General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines," SAE Technical Paper 640009, 1964, https://doi.org/10.4271/640009.Also In
References
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- Clarke A. E. 7 Symposium (International) on Combustion, Discussion 10, Section 8 730
- Clarke A. E. Odgers J. Ryan P. 8th Symposium (International) on Combustion
- Greenhough V. W. Lefebvre A. H. 6th Symposium (International) on Combustion New York Reinhold 1957 858
- Clarke J. S. ASME and IME Joint Conference on Combustion, Section 5 1955
- Chin et al ASME Report No. 58-A-107
- Eckert E. R. G. Livingood J. N. B. NACA Report TN 3010
- Clarke J. S. Hudson G. J. “Heavy Oil Burning,” Inst. Marine Engrs. 1959
- Clarke J. S. Lardge H. E. ASME Report 58-G.T.P. -13