1. 北京航空航天大学 航空科学与工程学院,北京,100191
2. 北京航空航天大学 航空器先进设计技术工业和信息化部重点实验室,北京,100191
向正平(1990-), 男, 硕士, 工程师, 研究方向:CFD仿真, 气动弹性力学.E-mail:xiangzhengping@163.com
戴玉婷(1985-), 女, 博士, 副教授, 主要研究方向:流固耦合、气动伺服弹性和主动控制.E-mail:yutingdai@buaa.edu.cn
纸质出版:2019
移动端阅览
向正平, 戴玉婷, 黄广靖. 旋转开槽圆筒式阵风发生器流场特性数值模拟[J]. 空气动力学学报, 2019, 37(6): 950-955.
XIANG Zhengping, DAI Yuting, HUANG Guangjing. Numerical simulation of flow field characteristics about rotating slotted cylinder gust generator[J]. 2019, 37(6): 950-955.
向正平, 戴玉婷, 黄广靖. 旋转开槽圆筒式阵风发生器流场特性数值模拟[J]. 空气动力学学报, 2019, 37(6): 950-955. DOI: 10.7638/kqdlxxb-2017.0175.
XIANG Zhengping, DAI Yuting, HUANG Guangjing. Numerical simulation of flow field characteristics about rotating slotted cylinder gust generator[J]. 2019, 37(6): 950-955. DOI: 10.7638/kqdlxxb-2017.0175.
在OpenFOAM开源代码框架下开发求解器,对旋转开槽圆筒式阵风发生器的动态等效升力系数进行数值模拟,与试验结果吻合较好,验证了求解器的正确性。在此基础上,对该型阵风发生器的下游流场扰动风速进行了数值模拟和流场分析,分析了开槽圆筒旋转方向、下游流场位置、减缩频率等因素对下游流场扰动阵风的影响规律。结果表明,开槽圆筒的旋转方向对中心线上下两侧流场产生不同影响,对中心线附近的流场干扰较大。阵风幅值的变化与减缩频率有关,当减缩频率值在0.2~0.25之间时,产生阵风的正弦特性最佳。该数值模拟的结果对阵风发生器试验装置的设计具有一定的指导意义。
A solver is developed under the OpenFOAM open source framework. The solver is validated by simulating the dynamic equivalent lift coefficient of the rotary slotted cylindrical gust generator
which is in good agreement with the experimental result. The numerical simulation and flow field analysis are carried out for the downstream flow field disturbance velocity. The effects of the rotation direction
the rotation frequency
and the flow velocity on the downstream flow field are analyzed. The results show that
the rotation direction of the cylinder has different effects on the flow field of the upper and lower sides of the center line with greater interference near the center line. The change of gust amplitude is related to the reduction frequency
and the sinusoidal characteristics of the gust are best when the reduced frequency is 0.2~0.25. The results of this numerical simulation have some guiding significance for the design of the test device.
ZHU B, LIU Q, QU X L, et al. Measurement and analysis of a gust generator flow field in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(6): 76-80. (in Chinese)
RAVEH D E. CFD-based models of aerodynamic gust response[J]. Journal of Aircraft, 2007, 44(3): 888-897.
CHE L, WU Z G, YANG C. Gust response and load alleviation of elastic wing and wind tunnel test[J]. Engineering Mechanics, 2011, 28(6): 212-218. (in Chinese)
YUAN G, LI A J, WANG C Q, Multiple rudders large civil aircraft gust alleviation system design[J]. Flight Mechanics, 2011, 29(4): 65-67. (in Chinese)
YANG J B, WU Z G, DAI Y T. Wind tunnel test of gust alleviation active control for flying wing configuration aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1): 184-192. (in Chinese)
ZONG N. The gust load analysis and alleviation design for a certain aircraft[C]//Proceedings of the National Doctoral Forum on Aeronautical Science and technology in 2016. (in Chinese)
DAI Y T, CHAO Y, WANG C. Strategy for robust gust response alleviation of an aircraft model[J]. Control Engineering Practice, 2016, 60: 211-217.
DOWELL E H, TANG D M, CIZMAS P G A. Experiments and analysis for a gust generator in a wind tunnel[J]. Journal of Aircraft, 1996, 33(1): 139-148.
LIU Z Q, SHI Z W, BAI P. Double wings miniature aircraft experimental study on horizontal gust response[J]. Journal of Experiments in Fluid Mechanics, 2009, 23(3): 54-57. (in Chinese)
SHI Z W, LIU Z Q, DING C. Flexible wing miniature aircraft experimental study on horizontal gust response[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(6): 1-5. (in Chinese)
BENNETT R M, GILMAN J. A wind-tunnel technique for measuring frequency-response functions for gust load analyses[J]. Journal of Aircraft, 1966, 3(6): 535-540.
MALIK M R, PLETCHER R H. A study of some turbulence models for flow and heat transfer in ducts of annular cross-section[J]. Journal of Heat Transfer, 1981, 103(1): 146-152.
BLCKNELL J, PARKER A G. A wind-tunnel stream oscillation apparatus[J]. Journal of Aircraft, 2015, 9(6): 446-447.
PARKER A G, BICKNELL J. Some measurements on dynamic stall[J]. Journal of Aircraft, 1974, 11(7): 371-374.
HAM N D, BAUER P H, LAWRENCE T L. Wind tunnel generation of sinusoidal lateral and longitudinal gusts by circulation of twin parallel airfoils[R]. NASA CR 1974-137547.
XU H Y, YE Z Y, HUO X L. Numerical calculation of flutter excitation system based on nested grid[J]. Acta Aerodynamica Sinca, 2010, 28(5): 536-539.
WANG T, SHI A M, YANG Y N. Characteristics of a new type of flutter excitation system[J]. Flight Mechanics, 2005, 23(1): 35-37.
YANG Z C, DANG H X, SUN Y J, et al. Numerical simulation of aerodynamic characteristics of a fixed small wing with a slotted rotating cylinder[J]. Engineering Mechanics, 2009, 26(11): 222-227. (in Chinese)
LIU Z R, ZOU H, LIU J S, et al. The influence of the slit angle of the slotted cylinder on the shedding vortex[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(1): 128-135. (in Chinese)
TANG D M, DOWELL E H. Response of a nonrotating rotor blade to lateral turbulence Part Ⅱ: Experiment[J]. Journal of Aircraft, 1995, 32(1): 154-160.
CIZMAS P G A, DOWELL E H, TANG D. Flow about a slotted cylinder-airfoil combination in a wind tunnel[J]. Journal of Aircraft, 1996, 33(4): 716-721.
MENTER F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA Journal, 1994, 32(8): 1598-1605.
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