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

机译:超音速氦气射流流动特性的实验与数值研究

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摘要

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 to simulate the total temperature ratio of heated jets and hence have the potential to provide inexpensive and reliable flow and acoustic measurements. Accurate knowledge of the mean flow is a crucial initial step for a complete understanding of the noise generation mechanisms. This study focuses on providing close comparisons between measured mean flow properties of helium-air mixture jets and results from simulations of similar mixed jets as well as heated air jets. Axisymmetric supersonic jets issuing from convergent and convergent-divergent nozzles are investigated, and the results show good agreement with heated air jet measurements. The flow properties are examined in detail to demonstrate the validity of simulating heat with the addition of helium. Excellent agreement is obtained in the presented data between the numerical predictions and the experiments, further justifying the helium addition methodology, as well as validating the frozen chemistry model used in the numerical simulations.
机译:按设计运行的高速亚音速和超音速高速喷气飞机是噪声的一个来源,目前尚未完全了解。氦气混合物可用于模拟加热射流的总温度比,因此有可能提供廉价而可靠的流量和声学测量结果。准确了解平均流量是全面理解噪声产生机制的关键的第一步。这项研究的重点是在氦-空气混合射流的实测平均流量特性与类似混合射流以及加热空气射流的模拟结果之间提供紧密的比较。研究了从会聚和会聚-发散喷嘴发出的轴对称超声速射流,结果与加热空气射流测量结果吻合良好。详细研究了流动特性,以证明添加氦气模拟热量的有效性。所提供的数据在数值预测和实验之间获得了极好的一致性,进一步证明了氦气添加方法的正确性,并验证了数值模拟中使用的冷冻化学模型。

著录项

  • 来源
    《AIAA Journal》 |2011年第1期|p.235-246|共12页
  • 作者单位

    NASA Langley Research Center, Hampton, Virginia 23681;

    Pennsylvania State University, University Park, Pennsylvania 16802;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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