Thrust performance of a flexible low-aspect-ratio pitching plate

被引:61
|
作者
Dai, Hu [1 ]
Luo, Haoxiang [1 ]
de Sousa, Paulo J. S. A. Ferreira [1 ]
Doyle, James F. [2 ]
机构
[1] Vanderbilt Univ, Dept Mech Engn, Nashville, TN 37235 USA
[2] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
基金
美国国家科学基金会;
关键词
WAKE STRUCTURE; OSCILLATING FOILS; FLAPPING FOIL; AIRFOIL; GENERATION; EFFICIENCY; PANEL;
D O I
10.1063/1.4764047
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We numerically investigate the hydrodynamic performance of an elastic plate of aspect ratio 0.54 and mass ratio 0.1 that pitches around its leading edge in a free stream at Reynolds number 640. It is found that for the rigid plate and the flexible plate with the first-mode deformation, the thrust coefficient nearly collapses onto the same curve when plotted against the Strouhal number that is defined using the tail excursion. Exceptions are found when the plate is overly flexible and higher deformation modes take place. On the other hand, the flexible plate has significantly higher power efficiency than the rigid plate at the same Strouhal number. Like the rigid plate, wake transition is observed for the flexible plate as the Strouhal number is varied. Specifically, at low Strouhal numbers (St < 0.28) the wake consists of a chain of interlocked horseshoe-shape vortices; at high Strouhal numbers (St > 0.28), the wake turns into two trains of closed vortex rings with hairpin legs. (C) 2012 American Institute of Physics. [http://dx.doi.org/10.1063/1.4764047]
引用
收藏
页数:9
相关论文
共 50 条
  • [41] LOW-ASPECT-RATIO WING CODE VALIDATION EXPERIMENT
    OLSEN, ME
    SEEGMILLER, HL
    AIAA JOURNAL, 1993, 31 (10) : 1744 - 1752
  • [42] OSCILLATORY CONVECTION IN LOW-ASPECT-RATIO CZOCHRALSKI MELTS
    ANSELMO, A
    PRASAD, V
    KOZIOL, J
    GUPTA, KP
    JOURNAL OF CRYSTAL GROWTH, 1993, 134 (1-2) : 116 - 139
  • [43] REMARKS ON LOW-ASPECT-RATIO CONFIGURATIONS IN SUPERSONIC FLOW
    LAGERSTROM, PA
    GRAHAM, ME
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (02): : 91 - &
  • [44] AERODYNAMIC INTERFERENCE FOR SUPERSONIC LOW-ASPECT-RATIO MISSILES
    NELSON, HF
    BOSSI, BW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1995, 32 (02) : 270 - 278
  • [45] Performance improvement of flapping propulsions from spanwise bending on a low-aspect-ratio foil
    Lin, Tianlong
    Xia, Wei
    Pecora, Rosario
    Wang, Kun
    Hu, Shuling
    OCEAN ENGINEERING, 2023, 284
  • [46] Comment on "Low-Aspect-Ratio Wing Aerodynamics at Low Reynolds Numbers"
    McCutchen, CW
    AIAA JOURNAL, 2006, 44 (04) : 924 - 924
  • [47] Formation of supercritical flow regions on low-aspect-ratio wings
    Dudin, G.N.
    Izvestiya Akademii Nauk. Mekhanika Zhidkosti I Gaza, 2005, (06): : 160 - 172
  • [48] Formation Flight of Low-Aspect-Ratio Wings at Low Reynolds Number
    Korkischko, Ivan
    Konrath, Robert
    JOURNAL OF AIRCRAFT, 2017, 54 (03): : 1025 - 1034
  • [49] Numerical investigation of low-aspect-ratio wings at low Reynolds numbers
    Cosyn, P.
    Vierendeels, J.
    JOURNAL OF AIRCRAFT, 2006, 43 (03): : 713 - 722
  • [50] Pressure and heat flux measurements on the surface of a low-aspect-ratio circular cylinder mounted on a ground plate
    Roediger, T.
    Knauss, H.
    Gaisbauer, U.
    Kraemer, E.
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VI, 2007, 96 : 121 - 128