Dual-Mode Scramjet Combustor: Numerical Analysis of Two Flowpaths

Ryan T. Milligan; Dean R. Eklund; J. Mitch Wolff; Mark Gruber; Tarun Mathur

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Dual-Mode Scramjet Combustor: Numerical Analysis of Two Flowpaths

机译：双模超燃燃烧室：两个流路的数值分析

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A preliminary numerical characterization of a U.S. Air Force Research Laboratory (AFRL) test facility was performed. Research cell 22 (RC22) is a supersonic wind-tunnel facility at AFRL. RC22 is presently simulating dual-mode combustion for circular (axisymmetric) combustors. Previous efforts in RC22 have studied combustion in rectangular flowpaths. The current effort in

机译：进行了美国空军研究实验室（AFRL）测试设施的初步数值表征。研究室22（RC22）是AFRL的超音速风洞设施。 RC22目前正在模拟圆形（轴对称）燃烧器的双模式燃烧。 RC22的先前研究已经研究了矩形流路中的燃烧。目前的努力

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《Journal of propulsion and power》 |2011年第6期|p.1317-1320|共4页
作者
Ryan T. Milligan; Dean R. Eklund; J. Mitch Wolff; Mark Gruber; Tarun Mathur;
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Taitech, Inc., Beavercreek, Ohio 45430;

U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;

U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;

U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;

Innovative Scientific Solutions, Inc., Dayton, Ohio 45440;

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Dual-Mode Scramjet Combustor: Numerical Analysis of Two Flowpaths

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