期刊文献+

极低风速标定系统密闭室洞壁影响研究

Research on Sealed Chamber Wall Effects in an Extremely Low Wind Speed Calibration Facility
下载PDF
导出
摘要 探头运动式极低风速标定系统密闭室洞壁干扰及前端壁扰动反射都可能对密闭室流场产生影响,从而影响标定精度。采用运动重叠网格技术,用URANS方程数值模拟密闭室流场,考察密闭室侧壁干扰、前端壁反射对流场和标定的影响。选择有洞壁和无洞壁情形计算密闭室流场,比较两种情形下的速度场;对于密闭室前端壁扰动反射问题,选择有前端壁和无前端壁两种边界条件,计算密闭室流场,比较不同时刻两种情形下的速度场。结果表明:洞壁干扰和前端壁反射引起的速度场偏差对标定的影响都在可接受范围内。 The side wall interference and disturbance reflection from the front end wall of a sealed chamber in an extremely low wind speed calibration facility operated by driving the probe in motion might have influence on the flow field inside the chamber,thus affecting the calibration accuracy.The moving overlapping grid technique is used in solving the URANS equations simulating the flow field in the chamber to investigate the effects of side-wall interference and the disturbance wave reflection from the front(upstream)end wall on the interior flow field and calibration.The flow fields in the cases with and without side walls are computed and compared.For the front end wall reflection of the strut rod disturbance,the boundary conditions with and without front end wall are used respectively in computing the flow field in the chamber,and the computed flow fields in the two cases are compared at several instants,respectively.The computed results show that the effects of velocity deviations caused by the wall interference and the front end wall reflection of disturbance on calibration accuracy are in an acceptable range.
作者 周廷波 田永强 刘佳航 张正科 张国彪 郗忠祥 高超 ZHOU Tingbo;TIAN Yongqiang;LIU Jiahang;ZHANG Zhengke;ZHANG Guobiao;XI Zhongxiang;GAO Chao(Facility Design and Instrumentation Institute,China Aerodynamics Research and Development Center,Mianyang 621000,China;National Key Laboratory of Science and Technology on Aerodynamic Design and Research,Northwestern Polytechnical University,Xi’an 710072,China)
出处 《航空工程进展》 CSCD 2022年第6期125-133,共9页 Advances in Aeronautical Science and Engineering
关键词 极低风速 标定系统 密闭室 洞壁干扰 前端壁反射 数值模拟 extremely low wind speed calibration facility sealed chamber wall interference front end wall reflection numerical simulation
  • 相关文献

参考文献4

二级参考文献25

  • 1陈德华,林俊,郭旦平,熊能.大型飞机高速气动力关键问题解决的技术手段及途径[J].流体力学实验与测量,2004,18(2):1-5. 被引量:13
  • 2陈德华,王维新,王晋军,周岭.2.4m跨声速风洞流场性能调试研究[J].空气动力学学报,2004,22(3):279-282. 被引量:9
  • 3黄勇,钱丰学,于昆龙,何彬华,畅利侠,林学东.基于柱状粗糙元的边界层人工转捩试验研究[J].实验流体力学,2006,20(3):59-62. 被引量:19
  • 4BEYERS M E. Unsteady wall interference in rotary tests [R]. AIAA-89-0049,1989.
  • 5ACCUM W E A. Interference effect in unsteady experiments [R]. AGARDograph 109,1966.
  • 6ACCUM W E A. Wall corrections for wings oscillating in wind tunnel of closed rectangular sections [R]. ARC R&M 3312,1959.
  • 7DRAKE D G. Wind tunnel interference for oscillating wings at transonic speed [R]. ARC 21489-01515,1959.
  • 8FORSCHING H. Wing tunnel wall corrections for unsteady flow applying steady wall adaptation and CFD techniques [R]. DLR Inst. Fur Aerolastik, Gttingen, Germany, 1991.
  • 9WEIBERG Z. Effect of tunnel walls on vortex breakdown location over delta wings [J]. AIAA J., 1992,30(6): 1584-1586.
  • 10HUMMEL D. Untersuchungen uber der aufplatzen der wirbel an schlanken deltaflugel [J]. Z.Flugwiss, 1965, 13(5): 158-168.

共引文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部