北京航空航天大学学报 ›› 1998, Vol. 24 ›› Issue (2): 181-184.

• 论文 • 上一篇    下一篇

双三角翼大迎角翼面压强分布与涡态相关分析

冯亚南, 郑波, 权少平   

  1. 北京航空航天大学 飞行器设计与应用力学系
  • 收稿日期:1996-12-09 出版日期:1998-02-28 发布日期:2010-09-28
  • 作者简介:女 62岁 教授 100083 北京
  • 基金资助:

    航空科学基金资助项目

Correlative Analysis between Pressure Distributions and VortexPattern of DoubleDelta Wings at High Angles of Attack

Feng Yanan, Zheng Bo, Quan Shaoping   

  1. Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics
  • Received:1996-12-09 Online:1998-02-28 Published:2010-09-28

摘要: 将双三角翼翼面测压试验结果与空间涡态观察测量结果进行了定性的相关对比分析,分析表明:垂直于双三角翼翼面的典型横截面上展向压强系数Cp分布与空间涡态有明显的对应关系,Cp分布的峰值数目反映了双三角翼的双涡态和单涡态,Cp峰值随α变化反映了涡强随α的变化,Cp峰值所在展向位置反映着涡核的展向位置,Cp峰形的平坦反映了涡的破裂.

Abstract: The pressure distributions on two models of doubledelta wing were measured in the low speed wind tunnel in BUAA.They are 75°/45° and 75°/60° doubledelta wings with sharp or round outboard leadingedge.The analysis indicates that two peaks of the pressure distributions on some typical cross sections of the doubledelta wing characterize the double vortices while the one peak of those characterize the single or merged vortex patterns.The position of the vortex core can be marked by the location of the spanwise pressure peak.The vortex breakdown can be displayed by the decrease of the pressure peak and flat pressure distribution with increasing angle of attack.The outboard leadingedge of the doubledelta wing being blunted causes inboard and outboard vortices close each other and stronger interaction.The pressure distributions and vortex breakdown positions will be unsymmetric about the centreline of the wing due to a side slip.All of the unsymmetric vortex flow characteristics that can be found on the correlative pressure distributions.

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