留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

吹气襟翼的螺旋桨滑流影响模拟

温庆 程志航 邱亚松 杨康智

温庆, 程志航, 邱亚松, 等. 吹气襟翼的螺旋桨滑流影响模拟[J]. 航空动力学报, 2023, 38(5):1123-1132 doi: 10.13224/j.cnki.jasp.20210294
引用本文: 温庆, 程志航, 邱亚松, 等. 吹气襟翼的螺旋桨滑流影响模拟[J]. 航空动力学报, 2023, 38(5):1123-1132 doi: 10.13224/j.cnki.jasp.20210294
WEN Qing, CHENG Zhihang, QIU Yasong, et al. Simulation of the effect of propeller slipstream on blowing control of flap[J]. Journal of Aerospace Power, 2023, 38(5):1123-1132 doi: 10.13224/j.cnki.jasp.20210294
Citation: WEN Qing, CHENG Zhihang, QIU Yasong, et al. Simulation of the effect of propeller slipstream on blowing control of flap[J]. Journal of Aerospace Power, 2023, 38(5):1123-1132 doi: 10.13224/j.cnki.jasp.20210294

吹气襟翼的螺旋桨滑流影响模拟

doi: 10.13224/j.cnki.jasp.20210294
详细信息
    作者简介:

    温庆(1983-),男,高级工程师,硕士,研究方向为气动力设计与分析

  • 中图分类号: V211.4

Simulation of the effect of propeller slipstream on blowing control of flap

  • 摘要:

    采用数值模拟方法,对内吹式附面层控制方案(吹气襟翼)的全机带螺旋桨滑流影响的气动力特性进行仿真计算,并与风洞试验结果对比。将4个螺旋桨区域单独划分网格,在各个域之间通过面搭接网格进行数据传递。采用基于多重参考坐标系的准定常方法和螺旋桨真实旋转的非定常方法,对升阻特性进行计算,并与风洞试验结果进行了对比。结果表明:准定常方法可以大致捕捉到升力特性曲线的发展趋势,但所计算的固定迎角下的升力系数具体数值与试验测试结果存在较大差距,该方法所捕捉的失速迎角也普遍小于试验测试结果,阻力特性也差距较大;非定常方法可以比较准确地捕捉到升力特性曲线发展趋势,对失速迎角及固定迎角下的升力系数具体数值捕捉也比较准确,阻力平均误差控制在15%以内。

     

  • 图 1  全流场网格分区示意图

    Figure 1.  Mesh partition diagram of full flow field

    图 2  各网格分区表面网格示意

    Figure 2.  Surface mesh of each mesh partition

    图 3  稳压腔与喷口示意图

    Figure 3.  Schematic diagram of pressure stabilizing cavity and nozzle

    图 4  风洞试验模型

    Figure 4.  Wind tunnel test model

    图 5  流量控制单元

    Figure 5.  Flow control unit

    图 6  无动力状态计算结果与试验测试结果对比

    Figure 6.  Comparison of calculated results with test results without power

    图 7  无动力状态各迎角下表面流线与截面速度云图

    Figure 7.  Velocity nephogram of surface streamlines and cross sections at different angles of attack without power

    图 8  带动力状态计算结果与试验测试结果对比

    Figure 8.  Comparison between calculation results and test results with power

    图 9  带动力状态各迎角下表面流线与截面速度云图

    Figure 9.  Surface streamlines and velocity counters of cross sections at different angles of attack with power

    图 10  非定常计算结果与试验测试结果对比

    Figure 10.  Comparison of unsteady calculation results with test results

    图 11  非定常数值模拟得到的螺旋桨旋转过程中的等涡量面(涡强度为1500 s−1)压力云图

    Figure 11.  Pressure of constant vorticity surface (vortex strength is 1500 s−1) during propeller rotation

  • [1] KELLER D, RUDNIK R. Numerical investigation of the dynamic behavior of a high-lift configuration with circulation control[C]// 33rd AIAA Applied aerodynamics conference. Dallas: AIAA Aviation, 2015: 2015-2571.
    [2] NILS B,ROLF R,CARSTEN L,et al. Aerodynamic effects of propeller slipstream on a wing with circulation control[J]. Journal of Aircraft,2015,52(5): 1422-1436. doi: 10.2514/1.C032901
    [3] MICHAEL M, WOLFGANG M. Towards the industrial application of active flow control in civil aircraft-an active highlift flap[C]//AIAA Applied aerodynamics conference. Atlanta: AIAA, 2014: 1508-1520.
    [4] GREENBLATT D,WYGNANSKI I J. The control of flow separation by periodic excitation[J]. Progress in Aerospace Sciences,2000,36(7): 487-545. doi: 10.1016/S0376-0421(00)00008-7
    [5] SOMMERWERK K,HAUPT M C. Design analysis and sizing of a circulation controlled cfrp wing with coanda flaps via CFD-CSM coupling[J]. CEAS Aeronautical Journal,2014,5(1): 95-108. doi: 10.1007/s13272-013-0093-9
    [6] BURNAZZI M,RADESPIEL R. Synergies between suction and blowing for active high-lift flaps[J]. Ceas Aeronautical Journal,2015,6(2): 305-318. doi: 10.1007/s13272-014-0146-8
    [7] RADESPIEL R,BURNAZZ M. Fundamentals in coanda flap design[J]. Notes on Numerical Fluid Mechanics & Multidiplinary Design,2015,127: 101-114.
    [8] ABZALILOV D. Maximizing the lift coefficient of a jet-blown contour[J]. Doklady Physics,2007,52(1): 63-66. doi: 10.1134/S1028335807010168
    [9] JABBAL M,LIDDLE S C,CROWTHER W J. Active flow control systems architectures for civil transport aircraft[J]. Journal of Aircraft,2010,47(6): 1966-1981. doi: 10.2514/1.C000237
    [10] LIDDLE S,CROWTHER W. Systems and certification issues for active flow control systems for seperation control on civil transport aircraft[J]. The Aeronautical Journal,2009,113(1147): 575-586.
    [11] 焦予秦,陆岩. 多段翼型吹气流动分离控制研究[J]. 应用力学学报,2015(2): 215-220. doi: 10.11776/cjam.32.02.A007

    JIAO Yuqin,LU Yan. Research on flow separation control on multi-element airfoil using air-blowing[J]. Chinese Journal of Applied Mechanics,2015(2): 215-220. (in Chinese) doi: 10.11776/cjam.32.02.A007
    [12] 刘沛清,崔燕香,屈秋林,等. 多段翼型前缘缝翼吹气流动与噪声控制数值研究[J]. 民用飞机设计与研究,2012(2): 6-12. doi: 10.19416/j.cnki.1674-9804.2012.02.003

    LIU Peiqing,CUI Yanxiang,QU Qiulin,et al. Computational investigation of the slat blowing and noise control for high-lift airfoil[J]. Civil Aircraft Design and Research,2012(2): 6-12. (in Chinese) doi: 10.19416/j.cnki.1674-9804.2012.02.003
    [13] 朱自强,吴宗成. 环量控制技术研究[J]. 航空学报,2016,37(2): 411-428.

    ZHU Ziqiang,WU Zongcheng. Study of the circulation control technology[J]. Acta Aeronautuca et Astronautica Sinica,2016,37(2): 411-428. (in Chinese)
    [14] 周涛,李亚林,党铁红. 民用飞机增升装置中的流动控制技术[J]. 民用飞机设计与研究,2013(4): 17-24, 28. doi: 10.3969/j.issn.1674-9804.2013.04.005

    ZHOU Tao,LI Yalin,DANG Tiehong. Flow control on high-lift devices of civil aircraft[J]. Civil Aircraft Design and Research,2013(4): 17-24, 28. (in Chinese) doi: 10.3969/j.issn.1674-9804.2013.04.005
    [15] 刘沛清,温瑞英,张国伟. 鸭翼展向吹气涡控技术增升特性研究[J]. 实验流体力学,2006,20(3): 39-44. doi: 10.3969/j.issn.1672-9897.2006.03.008

    LIU Peiqing,WEN Ruiying,ZHANG Guowei. A study on lift-enhancement with vortex control technique of canard-spanwise blowing[J]. Journal of Experiments in Fluid Mechanics,2006,20(3): 39-44. (in Chinese) doi: 10.3969/j.issn.1672-9897.2006.03.008
    [16] 孙卫平,杨康智,秦何军. 大型水陆两栖飞机吹气襟翼设计与分析验证[J]. 航空动力学报,2016,31(4): 903-909.

    SUN Weiping,YANG Kangzhi,QIN Hejun. Design and test of a jet flap for a large amphibian[J]. Journal of Aerospace Power,2016,31(4): 903-909. (in Chinese)
    [17] 郝璇,刘芳,王斌. 基于襟/缝翼吹气技术的短距起降飞行器增升策略的数值模拟研究[J]. 航空工程进展,2016,7(4): 408-419.

    HAO Xuan,LIU Fang,WANG Bin. The numerical simulation research on high lift enhancement strategies of stol aircraft based on flap and slat blowing[J]. Advances in Aeronautical Science and Engineering,2016,7(4): 408-419. (in Chinese)
    [18] 李志强,杜曼丽. Gao-Yong模型用于吹气环量控制翼型的研究[J]. 航空动力学报,2009,24(6): 1326-1331.

    LI Zhiqiang,DU Manli. Study of circulation control airfoil with blowing jet using Gao-Yong turbulence model[J]. Journal of Aerospace Power,2009,24(6): 1326-1331. (in Chinese)
    [19] 赵光银,姜裕标,王万波,等. 螺旋桨滑流对简单襟翼吹气控制的影响[J]. 航空动力学报,2021,36(3): 530-542.

    ZHAO Guangyin,JIANG Yubiao,WANG Wanbo,et al. Effect of propeller slipstream on blowing control of simple flap[J]. Journal of Aerospace Power,2021,36(3): 530-542. (in Chinese)
    [20] 麻蓉,高飞飞,颜洪,等. 螺旋桨飞机滑流非定常数值模拟研究[J]. 航空计算技术,2016,46(1): 27-30.

    MA Rong,GAO Feifei,YAN Hong,et al. Research on unsteady numerical simulation of propeller aircraft slipstream[J]. Aeronautical Computing Technique,2016,46(1): 27-30. (in Chinese)
    [21] 赵帅,段卓毅,李杰,等. 涡桨飞机螺旋桨滑流气动干扰效应及流动机理[J]. 航空学报,2019,40(4): 158-169.

    ZHAO Shuai,DUAN Zhuoyi,LI Jie,et al. Interference effects and flow mechanism of propeller slipstream for turboprop aircraft[J]. Acta Aeronautica et Astronautica Sinica,2019,40(4): 158-169. (in Chinese)
  • 加载中
图(11)
计量
  • 文章访问数:  206
  • HTML浏览量:  70
  • PDF量:  63
  • 被引次数: 0
出版历程
  • 收稿日期:  2021-06-10
  • 网络出版日期:  2023-03-14

目录

    /

    返回文章
    返回