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Simulation of Flame Spread and Turbulent Separated Flows in Solid Rockets

机译：固体火箭中火焰扩散和湍流分离流动的模拟

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《AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit》|2004年|P.1-11|共11页
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V. R; C. Unnikrishnan; B. N; T. Setoguchi;
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中图分类航空发动机（推进系统）;
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机译：具有侧壁壳体的固体火箭电机中复合推进剂湍流和扩散火焰的相互作用
2. Determining factor for the blowoff limit of a flame spreading in an opposed turbulent flow, in a narrow solid-fuel duct [J] . Nozomu Hashimoto, Harunori Nagata, Tsuyoshi Totani, Combustion and Flame . 2006,第3期

机译：狭窄的固体燃料管道中以相反湍流流动的火焰扩散极限的决定因素
3. Numerical simulation on gas-solid two-phase turbulent flow in FCC riser reactors(II) numerical simulation on the gas-solid two-phase turbulent flow [J] . Gao Jinsen, Xu Chunming, Lin Shixiong Chinese Journal of Chemical Engineering . 1998,第1期

机译：FCC立管反应器中气固两相湍流的数值模拟（II）气固两相湍流的数值模拟
4. Simulation of Flame Spread and Turbulent Separated Flows in Solid Rockets [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Propulsion Conference and Exhibit . 2004

机译：固体火箭中的火焰扩散和湍流分离流的仿真
5. Simulation of turbulent supersonic separated base flows using enhanced turbulence modeling techniques with application to an X-33 aerospike rocket nozzle system. [D] . Papp, John Laszlo. 2000

机译：使用增强的湍流建模技术对湍流超音速分离基流进行仿真，并将其应用于X-33气钉火箭喷嘴系统。
6. Advancing predictive models for particulate formation in turbulent flames via massively parallel direct numerical simulations [O] . Fabrizio Bisetti, Antonio Attili, Heinz Pitsch -1

机译：通过大规模并行直接数值模拟改进湍流火焰中颗粒形成的预测模型
7. Sounding Rocket Microgravity Experiments Elucidating Diffusive and Radiative Transport Effects on Flame Spread over Thermally-Thick Solids [O] . Olson Sandra L., Tang L., Bhattacharjee S., 2003

机译：探空火箭微重力实验，阐明了火焰在热厚固体上的扩散和辐射传输效应
8. Solid Fuel Flame Spread and Mass Burning in Turbulent Flow. [R] . Zhou, L. 1992

机译：湍流中固体燃料火焰蔓延和质量燃烧。

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