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Effect of burner design variables on performance of 16-inch diameter ram-jet combustor using gaseous-hydrogen fuel

机译：燃烧器设计变量对使用气态氢燃料的16英寸直径喷射式燃烧室性能的影响

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An evaluation of the effect of geometric design variables on the performance of a16-inch-diameter ram-jet combustor total pressures from 7 to 44 inches of mercury absolute. Equivalent ratio was varied from 0.1 to 1.0 at a combustor inlet temperature of 1100 degrees R.

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Krull, H George; Burley, Richard R;
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年度 1957
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Computational investigation of an ethylene-fueled supersonic combustor assisted by a porous cylindrical burner [J] . Lee Wei-Shen, Pan Kuo-Long Aerospace science and technology . 2020,第Deca期

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3. The design and performance of a RP-3 fueled high temperature rise combustor based on RQL staged combustion [J] . Jianzhong Li, Jian Chen, Wu Jin, Energy . 2020,第Octa15期

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5. Evaluation of the Performance of a Variable Geometry Low-Swirl Burner Operated on Simulated Renewable Fuels in a Boiler Environment. [D] . Kirksey, Nathan James. 2014

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6. Influence of Chemical Kinetics on Predictions of Performance of Syngas Production From Fuel-Rich Combustion of CO2/CH4 Mixture in a Two-Layer Burner [O] . Junrui Shi, Mingming Mao, Houping Li, 2019

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7. Alternative Fuels: Burner Concepts and Emission Characteristics of a Silo Combustor [O] . W. Krockow, H. Schabbehard 1982

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Effect of burner design variables on performance of 16-inch diameter ram-jet combustor using gaseous-hydrogen fuel

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