219 非対称ノズルから噴出される超音速噴流の干渉特性

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タイトル別名
  • Interference Characteristics of Supersonic Jets Issuing from Asymmetric Nozzle
  • ヒタイショウ ノズル カラ フンシュツサレル チョウオンソク フンリュウ ノ

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抄録

In this paper, the structure and behavior of the supersonic jets issuing from asymmetric single nozzle which had oblique outlet and two parallel asymmetric nozzles were studied mainly by the flow visualization. The flow visualization of mean and instantaneous flows with time were conducted by the schieren and shadowgraph methods, moreover mean total pressure distributions were measured. It was clarified that effect of oblique nozzle outlet on structure of pseudo-shock wave, and relation between distance of two parallel asymmetric nozzles and interference characteristics of two oblique jets.

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