Low-frequency vortex oscillation around slender bodies at high angles-of-attack

被引:18
|
作者
Ma, Bao-Feng [1 ]
Liu, Tong-Xin [1 ]
机构
[1] Beihang Univ, Key Lab Fluid Mech, Minist Educ, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
ASYMMETRIC VORTICES; CIRCULAR-CYLINDERS; OGIVE-CYLINDER; FLOW; BODY; REVOLUTION; SEPARATION; MODEL; WAKE;
D O I
10.1063/1.4895599
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Low-frequency unsteadiness of vortices over an ogive-cylinder body was studied using numerical simulation and Dynamic Mode Decomposition (DMD). The results revealed that the vortices over the fore-body of the slender body can exhibit vortex oscillation with a non-dimensional frequency of 0.054 at 70 degrees angle-of-attack, but the flow pattern over the aft-body downstream is Karman vortex shedding. The vortex oscillation induces larger sectional side-forces on the body than vortex shedding. The DMD analysis for the sectional flow fields at various sections shows that the most energetic mode corresponds to the vortex oscillation at the fore-body and the vortex shedding at the aft-body except the mode for a mean flow, and the associated frequencies are identical to the ones of the sectional side-forces obtained by Fourier transformation. (C) 2014 AIP Publishing LLC.
引用
收藏
页数:7
相关论文
共 50 条
  • [31] Effects of forced asymmetric transition on vortex asymmetry around slender bodies
    Ma, Bao-Feng
    Deng, Xue-Ying
    Chen, Ying
    AIAA JOURNAL, 2007, 45 (11) : 2671 - 2676
  • [32] LOW-FREQUENCY OSCILLATION - REPLY
    SCHLESINGER, ME
    RAMANKUTTY, N
    NATURE, 1994, 372 (6506) : 508 - 509
  • [33] GROUND EFFECT ON SLENDER WINGS AT MODERATE AND HIGH ANGLES OF ATTACK
    EREL, J
    WEIHS, D
    JOURNAL OF AIRCRAFT, 1986, 23 (05): : 357 - 358
  • [34] VORTEX UNSTEADINESS ON SLENDER BODIES AT HIGH-INCIDENCE
    ERICSSON, LE
    JOURNAL OF SPACECRAFT AND ROCKETS, 1987, 24 (04) : 319 - 326
  • [35] Vortex-Induced Vibration and Frequency Lock-In of an Airfoil at High Angles of Attack
    Besem, Fanny M.
    Kamrass, Joshua D.
    Thomas, Jeffrey P.
    Tang, Deman
    Kielb, Robert E.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2016, 138 (01):
  • [36] VORTEX-INDUCED VIBRATION AND FREQUENCY LOCK-IN OF AN AIRFOIL AT HIGH ANGLES OF ATTACK
    Besem, Fanny M.
    Kamrass, Joshua D.
    Thomas, Jeffrey P.
    Tang, Deman
    Kielb, Robert E.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 7B, 2014,
  • [37] Vortex dynamics of axisymmetric cones at high angles of attack
    Shahriar, Al
    Kumar, Rajan
    Shoele, Kourosh
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2023, 37 (03) : 337 - 356
  • [38] Vortex dynamics of axisymmetric cones at high angles of attack
    Al Shahriar
    Rajan Kumar
    Kourosh Shoele
    Theoretical and Computational Fluid Dynamics, 2023, 37 : 337 - 356
  • [39] YAW DAMPING OF ELLIPTIC BODIES AT HIGH ANGLES OF ATTACK
    BLAKE, WB
    BARNHART, BP
    JOURNAL OF AIRCRAFT, 1990, 27 (07): : 670 - 672
  • [40] Investigation of asymmetric flow past a slender body at high angles of attack
    Obeid, Osama
    AlQadi, Ibraheem
    AlMutairi, Jaber
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2019, 33 (05) : 481 - 508