Wavelet analysis of transonic buffet on a two-dimensional airfoil with vortex generators

被引:18
作者
Kouchi, Toshinori [1 ]
Yamaguchi, Shingo [1 ]
Koike, Shunske [2 ]
Nakajima, Tsutomu [3 ]
Sato, Mamoru [3 ]
Kanda, Hiroshi [3 ]
Yanase, Shinichiro [1 ]
机构
[1] Okayama Univ, Dept Mech & Syst Engn, Kita Ku, Tsushimanaka 3-1-1, Okayama 7008530, Japan
[2] JAXA, Aeronaut Technol Directorate, Next Generat Aeronaut Innovat Hub Ctr, Jindaiji Higashi 7-44-1, Chofu, Tokyo 1828522, Japan
[3] JAXA, Aeronaut Technol Directorate, Aerodynam Res Unit, Jindaiji Higashi 7-44-1, Chofu, Tokyo 1828522, Japan
关键词
28;
D O I
10.1007/s00348-016-2261-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
We visualized the shock buffets on a two-dimensional transonic airfoil with and without vortex generators (VGs) by using a fast-framing focusing schlieren imaging. The focusing schlieren visualization showed that the flow three-dimensionality around the airfoil became remarkable with installing the VGs. This implies that narrow depth of focus of imaging systems was a key to accurately capture the characteristics of the shock oscillation due to the buffet for the cases with VGs. The time-resolved imaging also revealed that non-periodic components were included in the shock oscillation due to the buffet for the cases with VGs. This prevented Fourier analysis from being applied. We used wavelet analysis to extract the characteristic of the shock oscillation for the cases with VGs. The wavelet spectrograms revealed that the low-frequency oscillation having the buffet frequency was still included intermittently in the shock oscillation even when VG controlled the buffet. The rate of appearing the low-frequency oscillation increased with increasing both the interval between VGs and the angle of attack.
引用
收藏
页数:15
相关论文
共 29 条
  • [1] [Anonymous], 1958, TN4363 NACA
  • [2] Origin of transonic buffet on aerofoils
    Crouch, J. D.
    Garbaruk, A.
    Magidov, D.
    Travin, A.
    [J]. JOURNAL OF FLUID MECHANICS, 2009, 628 : 357 - 369
  • [3] Harris C. D., 1990, TP2969 NASA
  • [4] Numerical investigation of unsteady wave phenomena for transonic airfoil flow
    Hermes, V.
    Klioutchnikov, I.
    Olivier, H.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 25 (01) : 224 - 233
  • [5] Ito Y, 2016, J AIRCRAFT IN PRESS
  • [6] Experimental Study of Shock Oscillation over a Transonic Supercritical Profile
    Jacquin, L.
    Molton, P.
    Deck, S.
    Maury, B.
    Soulevant, D.
    [J]. AIAA JOURNAL, 2009, 47 (09) : 1985 - 1994
  • [7] Koike S., 2015, 20151237 AIAA
  • [8] Koike S, 2013, 05082 APISAT2013
  • [9] Kouchi T, MODIFIED LEES TRANSO
  • [10] Focusing-schlieren visualization in a dual-mode scramjet
    Kouchi, Toshinori
    Goyne, Christopher P.
    Rockwell, Robert D.
    McDaniel, James C.
    [J]. EXPERIMENTS IN FLUIDS, 2015, 56 (12) : 1 - 14