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Development of Sub-scale Combustor for a Liquid Rocket Engine Using Swirl Injector with External Mixing

机译：用外部混合使用旋流注射器的液体火箭发动机亚级燃烧器的开发

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1. Full-length visualisation of liquid oxygen disintegration in a single injector sub-scale rocket combustor [J] . Suslov Dmitry I., Hardi Justin S., Oschwald Michael Aerospace science and technology . 2019,第MARa期

机译：单个喷射器小规模火箭燃烧室中液氧分解的全长可视化
2. Longitudinal combustion instability of a pintle injector for a liquid rocket engine combustor [J] . Sakaki Kazuki, Funahashi Tomokazu, Nakaya Shinji, Combustion and Flame . 2018,第AUGa期

机译：液体火箭发动机燃烧室销轴喷射器的纵向燃烧不稳定性
3. Combustion Characteristics of Ethanol/Liquid-Oxygen Rocket-Engine Combustor with Planar Pintle Injector [J] . Kazuki Sakaki, Hiromitsu Kakudo, Shinji Nakaya, Journal of propulsion and power . 2017,第2期

机译：平面针形喷油器的乙醇/液氧火箭发动机燃烧室燃烧特性
4. Modal Analysis of Combustion Oscillation Based on High-speed Measurements ofCH* chemiluminescence for a Liquid Rocket Engine Model Combustor with a Pintle Injector [C] . Kyo Sugihara, Tomokazu Funahashi, Shinji Nakaya, The 9th Asian joint conference on propulsion and power: conference guide . 2018

机译：基于 r nCH *化学发光的高速测量的带有枢轴喷射器的液体火箭发动机模型燃烧器的燃烧振荡模态分析
5. Development of a liquid oxygen facility for rocket engine injector performance testing. [D] . Mulkey, Henry W. 2010

机译：开发用于火箭发动机喷油器性能测试的液氧设备。
6. The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor [O] . Simon Gövert, Daniel Mira, Jim B. W. Kok, -1

机译：部分预混合和热损失对旋流稳定型燃气轮机模型燃烧器反应流场预测的影响
7. Full-length visualisation of liquid oxygen disintegration in a single injector sub-scale rocket combustor [O] . Dmitry I. Suslov, Justin S. Hardi, Michael Oschwald 2019

机译：单个注射器亚级火箭燃烧器中液体氧崩解的全长可视化
8. Comparison of the Performance of 1st Order and 2nd Order Turbulence Models when Solving the RANS Equations in Reproducing the Liquid Film Length Unsteady Response to Momentum Flux Ratio in Gas-Centered Swirl-Coaxial Injectors in Rocket Engine Applications [R] . Villasmil, L. A., Himansu, A. 2012

机译：在火箭发动机应用中以气体为中心的旋涡同轴喷射器再现液膜长度对动量通量比的非稳态响应中求解RaNs方程时一阶和二阶湍流模型的性能比较

Development of Sub-scale Combustor for a Liquid Rocket Engine Using Swirl Injector with External Mixing

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