跨超声速开式空腔流激振荡模态预估分析

Prediction and analysis of flow oscillation modes inside open cavities at transonic or supersonic speeds

  • 摘要: 以Rossiter和Heller的开式空腔流激振荡物理机制与模态预估分析方法为基础,采用量纲分析方法,对描述腔体流激振荡特性的参数进行无量纲处理后进行了分析,并提出了一种新的激振频率预测半经验公式中常数值选取方法,通过风洞试验结果和国外文献结果进行验证,表明该方法基本可行。

     

    Abstract: Unsteady flow characteristics and complex flow-field structures are main phenemena as transonic or supersonic speed flow past open cavities. Physical mechanism and rational predicted method of flowoscillations in open cavities remains as a research hotspot for years. Many explanations on the flowoscillation in the open cavities are proposed now and then. The method presented by Rossiter is the most feasible, which indicates a theory model for sound occurrence and feedback in the open cavities. The method recuenes that some vortices are generated from flow separation in shear-layer over the open cavity, then the vortices move to the rear region of the cavity at some velocity, and impingement of the vortex and the rear-wall of the cavity occurs. Some sound waves spread abroad to the cavity fore-wall, which induces some new vortices generation, and the vortices shed, move and impinge on the cavity rear-wall. New sound waves occur. Therefore, this paper presents some analysis of the parameters describing flow-oscillations based on non-dimension analysis method according to predicted method on self-sustained flow-oscillation modes in open cavities. A new selected method on the constant value in Rossiter's and Heller's semi-experience formula is presented. The result indicates that the method is feasible by comparing with wind-tunnel experimental result and overseas references.

     

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