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压电振子激励流场的数值模拟
  • ISSN号:1001-4055
  • 期刊名称:推进技术
  • 时间:2013.8.15
  • 页码:1016-1022
  • 分类:V231.1[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术]
  • 作者机构:[1]南京航空航天大学能源与动力学院,江苏南京210016
  • 相关基金:国家自然科学基金(51106073); 航空基金资助项目(2011ZB52020)
  • 相关项目:压电谐振风扇激励非定常涡环流动与换热特性研究
中文摘要:

为了得到多个压电振子的相干性和涡系之间相互干涉的流场信息,探索间距和相位差等因素对多个压电振子耦合流场的影响效果,本文对单个与多个压电振子的非定常流场特性进行了数值模拟研究。结果表明,压电振子振动时,流场中出现了速度涡区,单个振子的涡系发展最充分,流场中速度峰值达4m/s,三个振子的垂直方向作用范围最大,但速度峰值只有2.8m/s;振子振幅为A,振子间距在1A~4A,流场掺混效果与振子间距成正比,有1/2相位差时流场掺混效果优于无相位差的情况;多个振子产生的耦合射流效果在适当的间距与相位差下好于单个振子产生的射流。

英文摘要:

In order to get the coherence between multiple fans and the flow field information of vortex system and to study the effects of different space and phase difference on flow field in multiple - fan cases, numerical simulation was carried out to illustrate unsteady flow characteristics of multiple fans. The results show that velocity vortex is observed in the flow field when the fans vibrate. The vortex system of single fan flow field is most fully developed, and the peak velocity is 4m/s. The widest action range in vertical direc- tion is observed in the three -fan flow field, while its peak velocity is only 2.8m/s. The oscillator ampli- tude was defined as A. When the oscillator spacing ranges from 1A to 4A ,the flow field mixing effectiveness is proportional to the space between two fans, and the mixing effectiveness in the flow field with 1/2 phase difference between two fans is better than that without phase difference. The coupling effect of multiple jets with appropriate space and phase difference is better than the flow field of a single fan.

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期刊信息
  • 《推进技术》
  • 中国科技核心期刊
  • 主管单位:中国航天科工集团公司
  • 主办单位:北京动力机械研究所
  • 主编:郑日恒
  • 地址:北京7208信箱26分箱
  • 邮编:100074
  • 邮箱:tjjs@sina.com
  • 电话:010-68376141 68191522
  • 国际标准刊号:ISSN:1001-4055
  • 国内统一刊号:ISSN:11-1813/V
  • 邮发代号:
  • 获奖情况:
  • 国内外数据库收录:
  • 被引量:9176