Exploring cause of asymmetric vortex flow over slender circular cone at high angle of attack

被引：0
|
作者：
Meng, Xuanshi [1 ]
Qiao, Zhide [1 ]
Gao, Chao [1 ]
Luo, Shijun [2 ]
Liu, Feng [2 ]
机构：
[1] National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, Xi'an 710072, China
[2] Department of Mechanical and Aerospace Engineering, University of California, Irvine 92697-3975, United States
来源：
Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University | 2010年 / 28卷 / 05期
关键词：
8;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：655 / 659
相关论文
共 50 条
  • [41] Experimental study of asymmetric vortex control at high angle of attack with synthetic jet
    Li, Binbin
    Jiang, Yubiao
    Gu, Yunsong
    Cheng, Keming
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2015, 36 (03): : 764 - 771
  • [42] HYPERSONIC BOUNDARY LAYER FLOW OVER A SHARP CONE AT SMALL ANGLE OF ATTACK
    DWYER, HA
    BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1969, 14 (11): : 1090 - &
  • [43] Reinforcement learning-based plasma flow control of asymmetric vortices over a slender body at high angles of attack
    Zheng, Borui
    Gao, Peng
    Liu, Haodong
    Liu, Yichi
    An, Shuaimin
    Wei, Yilun
    Chen, Jiayin
    Liu, Fengqing
    Wu, Hongwei
    Huang, Bangdou
    Yu, Minghao
    Ge, Chang
    PHYSICS OF FLUIDS, 2025, 37 (03)
  • [44] Optimized plasma actuation on asymmetric vortex over a slender body
    Long, Yuexiao
    Li, Huaxing
    Meng, Xuanshi
    Hu, Haiyang
    APPLIED PHYSICS LETTERS, 2018, 112 (01)
  • [45] TRANSVERSE CURVATURE EFFECTS ON A SLENDER CONE WITH HEAT-TRANSFER AND ANGLE OF ATTACK
    KUMAR, P
    JAIN, AC
    ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1983, 63 (12): : 589 - 598
  • [46] Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration
    Chen, Mingqian
    Liu, Peiqing
    Guo, Hao
    Qu, Qiulin
    JOURNAL OF AIRCRAFT, 2016, 53 (01): : 217 - 230
  • [47] Asymmetric Vortices Around a Body in a High angle of attack Supersonic Flow
    Park, Mee-Young
    Kim, Wan-Sub
    Kim, Sangho
    Park, Soo Hyung
    Lee, Jae-Woo
    JOURNAL OF THE KOREAN PHYSICAL SOCIETY, 2009, 55 (05) : 2159 - 2165
  • [48] Numerical study of combined perturbation control of asymmetric vortices on a slender body of revolution at high angle of attack
    Feng, Feng
    Liu, Yang
    Sun, De-Jun
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2010, 28 (04): : 365 - 371
  • [49] COMPARISON OF HIGH-ANGLE-OF-ATTACK SLENDER-BODY THEORY AND EXACT-SOLUTIONS FOR POTENTIAL FLOW OVER AN ELLIPSOID
    HEMSCH, MJ
    JOURNAL OF AIRCRAFT, 1990, 27 (06): : 569 - 571
  • [50] SUPPRESSION OF ASYMMETRY OF THE VORTEX FLOW BEHIND A CIRCULAR CONE AT HIGH-INCIDENCE
    STAHL, W
    AIAA ATMOSPHERIC FLIGHT MECHANICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 231 - 236
12345