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Experimental and Numerical Investigation of Flow Properties of Supersonic Helium-Air Jets

机译:超声氦气喷射流动性能的实验性和数值研究

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Heated high speed subsonic and supersonic jets operating on- or off-design are a source of noise that is not yet fully understood. Helium-air mixtures can be used in the correct ratio to simulate the total temperature ratio of heated air jets and hence have the potential to provide inexpensive and reliable flow and acoustic measurements. This study presents a combination of flow measurements of helium-air high speed jets and numerical simulations of similar helium-air mixture and heated air jets. Jets issuing from axisymmetric convergent and convergent-divergent nozzles are investigated, and the results show very strong similarity with heated air jet measurements found in the literature. This demonstrates the validity of simulating heated high speed jets with helium-air in the laboratory, together with the excellent agreement obtained in the presented data between the numerical predictions and the experiments. The very close match between the numerical and experimental data also validates the frozen chemistry model used in the numerical simulation.
机译:加热的高速子系统和超音速喷射操作,操作或非设计是尚未完全理解的噪声源。氦气混合物可以以正确的比率使用,以模拟加热空气喷射的总温度比,因此有可能提供廉价且可靠的流动和声学测量。本研究介绍了氦气高速喷射的流量测量和类似氦气混合物和加热空气喷射的数值模拟的组合。研究了从轴对称收敛和会聚 - 发散喷嘴发出的喷射,结果表现出在文献中发现的加热空气喷射测量非常强烈的相似性。这证明了在实验室中使用氦气模拟加热的高速喷射的有效性,以及在数值预测和实验之间所获得的数据中获得的优秀协议。数值和实验数据之间的非常紧密的匹配还验证了数值模拟中使用的冷冻化学模型。

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