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Flow visualization and experimental optimization of three inlet-side-dump liquid-fuel ramjet combustors

机译：三种进气侧倾卸式液体燃料冲压喷射燃烧器的流动可视化和实验优化

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Approved for public release; distribution is unlimited.

机译：批准公开发布；发行是无限的。

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Salyer Ronald Frank;
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年度 1993
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原文格式 PDF
正文语种 en_US
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1. Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow [J] . Shi Lei, Zhao Guojun, Yang Yiyan, Aerospace science and technology . 2020,第Apra期

机译：总进气量低的煤油供油的RBCC燃烧室中喷射器到冲压发动机模式过渡的实验研究
2. Experimental Investigation of the Flow Inside a Water Model of a Gas Turbine Combustor: Part 2—Higher Order Moments and Flow Visualization [J] . J. J. McGuirk, J. M. L. M. Palma Journal of Fluids Engineering . 1995,第3期

机译：燃气轮机燃烧器水模型内部流动的实验研究：第2部分-高阶矩和流动可视化
3. Experimental investigation of the flow inside a water model of a gas turbine combustor: part 2--higher order moments and flow visualization [J] . J. J. McGuirk, J. M. L. M. Palma Journal of Fluids Engineering: Transactions of the ASME . 1995,第3期

机译：燃气轮机燃烧器水模型流动的实验研究：第2部分 - 高阶矩和流量可视化
4. Combustion of hydrogen in hot air flows within LAPCAT-Ⅱ Dual Mode Ramjet combustor at Onera-LAERTE facility-Experimental and Numerical Investigation [C] . Axel VINCENT-RANDONNIER, Yann MOULE, Marc FERRIER AIAA international space planes and hypersonic systems and technologies conference;AIAA aviation forum . 2014

机译：Onera-LAERTE设施的LAPCAT-Ⅱ双模Ramjet燃烧室中热气流中氢的燃烧-实验和数值研究
5. Numerical modeling of multiphase turbulent recirculating flows in a ramjet combustor [D] . Moss, Glenn Alan 1989

机译：冲压喷气发动机燃烧室中多相湍流再循环流动的数值模拟
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. Correction: Experimental Characterization of a Solid-Fuel Ramjet Combustor at Flight-Relevant Conditions [O] . Jay V. Evans, William C. Senior, Rohan Gejji, 2020

机译：校正：在飞行相关条件下的固体燃料拉米特燃烧器的实验表征

Flow visualization and experimental optimization of three inlet-side-dump liquid-fuel ramjet combustors

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