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AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT SIMULATION OF MIXING PROCESS GAS DYNAMICS IN THE GTE COMBUSTOR

机译:GTE燃烧室混合气体动力学的飞机火箭发动机设计与仿真。

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摘要

We presented the results of simulating gas dynamics of the processes of mixing a single jet and a system of jets. The calculations were carried out in the programming complex of the ANSYS finite-element analysis. The calculation results were compared with the experimental data for the dilution zone in a tubular combustor of the counter-flow scheme.
机译:我们介绍了模拟混合单个喷嘴和喷嘴系统过程的气体动力学的结果。计算是在ANSYS有限元分析的编程复合体中进行的。将计算结果与逆流方案的管状燃烧室中稀释区的实验数据进行了比较。

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