Research and Development of Turbo Jet Combustor on HST Programme in Japan
説明
<jats:p>The research and development of a turbo jet combustor for a Mach 3 class supersonic transport is underway, as well as the other components of the HST programme in JAPAN. This research and development aims finally at achieving a combustor exit temperature of 1973K while maintaining low NOx levels, high durability, and good exit temperature distribution.</jats:p> <jats:p>This paper describes the interim status of the combustor research and development, in particular, the liner cooling system and exit temperature distribution control technique.</jats:p>
収録刊行物
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- Volume 3C: General
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Volume 3C: General 1993-05-24
American Society of Mechanical Engineers