航空学报 > 1990, Vol. 11 Issue (10): 480-483

涡量场测量

王祖丰, 忻鼎定   

  1. 北京航空航天大学
  • 收稿日期:1990-02-05 修回日期:1990-04-25 出版日期:1990-10-25 发布日期:1990-10-25

MEASUREMENTS OF VORTICITY FIELD

Wang Zufeng, Xin Dingding   

  1. Beijing University of Aeronautics and Astronautics
  • Received:1990-02-05 Revised:1990-04-25 Online:1990-10-25 Published:1990-10-25

摘要: <正> The space .distributions of vorticity were measured by using a vorticimctcr (vorti-city probe) in the field induced by a vortex shedding from the wing-tip of a rectangular wing under different angles of attack. The results show that the vorticimetcr having the advantages of high sensitivity, simpler calibration process and easiness to use, is capable of measuring the vorticity directly, and finding out the center trace of the vortex core exactly. Through the measurements, a counter rotating vortex with a center strength of 1/17 to that of the main wing-tip vortex existing nearby is discovered. The center vorticity would decay substantially as the main wing-tip vertex moves down-stream. For instance, the peak vorticity at x = 2.5c (c, the chord length) will decay to about 25% of that at x = 0.1c, while its scale remains almost unchanged. At the cross-section x = 0.1c, the scale of the wing-tip vortex was about 0.2c spanwisc and-0.18c along the longtudinal direction. Finally, the strengths of a pair of in

关键词: 测量, 涡流, 流场

Abstract: The space .distributions of vorticity were measured by using a vorticimctcr (vorti-city probe) in the field induced by a vortex shedding from the wing-tip of a rectangular wing under different angles of attack. The results show that the vorticimetcr having the advantages of high sensitivity, simpler calibration process and easiness to use, is capable of measuring the vorticity directly, and finding out the center trace of the vortex core exactly. Through the measurements, a counter rotating vortex with a center strength of 1/17 to that of the main wing-tip vortex existing nearby is discovered. The center vorticity would decay substantially as the main wing-tip vertex moves down-stream. For instance, the peak vorticity at x = 2.5c (c, the chord length) will decay to about 25% of that at x = 0.1c, while its scale remains almost unchanged. At the cross-section x = 0.1c, the scale of the wing-tip vortex was about 0.2c spanwisc and-0.18c along the longtudinal direction. Finally, the strengths of a pair of interacting co-rotational vortices were measured. The rcaults reveal that both their locations and the central strength vary significantly as the two wings with each producing a tip vortex approach each other. At the cross-section x = 0.3c, these two co-rotational vortices with 0.195c apart arc found to wind up clearly.

Key words: measurement, vortex, flow field