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美国政府科技报告
>Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and fuel-cooled stage-type flame holders on J35-A-5 turbojet engine / Richard L. Golladay and Harry E. Bloomer
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Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and fuel-cooled stage-type flame holders on J35-A-5 turbojet engine / Richard L. Golladay and Harry E. Bloomer
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机译：J35-a-5涡轮喷气发动机/ Richard L. Golladay和Harry E. Bloomer的29英寸直径尾管燃烧器的高度性能和操作特性，带有多个燃油系统和燃油冷却级式火焰支架
An investigation of tail-pipe burning was conducted in the NACA Lewis altitude wind tunnel with a full-scale turbojet engine and an 29-inch-diameter tail-pipe burner. Effects of fuel distribution and number and arrangement of stages on performance and operational characteristics of several fuel-cooled flame holders are presented and discussed. Operation with a three-stage flame holder having the large stage upstream was the most efficient. Combustion efficiency was slightly increased at high altitudes by injecting fuel upstream of the flame holder.
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