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跨超声速开式空腔流激振荡模态预估分析

杨党国 祝静 李建强 梁锦敏 张诣

空气动力学学报Issue(3):369-375,7.
空气动力学学报Issue(3):369-375,7.DOI:10.7638/kqdlxxb-2012.0126

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

杨党国 1祝静 2李建强 1梁锦敏 3张诣4

作者信息

  • 1. 中国空气动力研究与发展中心 空气动力学国家重点实验室,绵阳 621000
  • 2. 中国空气动力研究与发展中心 高速空气动力研究所,绵阳 621000
  • 3. 重庆大学 通信工程学院,重庆 400030
  • 4. 中国空气动力研究与发展中心 高速空气动力研究所,绵阳 621000
  • 折叠

摘要

Abstract

Unsteady flow characteristics and complex flow-field structures are main phenemena as tran-sonic 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-oscilla-tion 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-di-mension analysis method according to predicted method on self-sustained flow-oscillation modes in open cavi-ties.A new selected method on the constant value in Rossiter′s and Heller′s semi-experience formula is pres-ented.The result indicates that the method is feasible by comparing with wind-tunnel experimental result and overseas references.

关键词

开式空腔/流激振荡/模态预估/物理机制/预估方法

Key words

open cavities/flow oscillation/predicted modes/physical mechanism/predicted method

分类

航空航天

引用本文复制引用

杨党国,祝静,李建强,梁锦敏,张诣..跨超声速开式空腔流激振荡模态预估分析[J].空气动力学学报,2014,(3):369-375,7.

基金项目

国家自然科学基金(11272335);气动预研基金 ()

空气动力学学报

OA北大核心CSCDCSTPCD

0258-1825

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