Three-dimensional effect on transonic rectangular cavity flows

被引:19
|
作者
Chung, KM [1 ]
机构
[1] Natl Cheng Kung Univ, Aerosp Sci & Technol Res Ctr, Tainan 711, Taiwan
关键词
Vortex; Pressure Gradient; Mach Number; Surface Pressure; Peak Pressure;
D O I
10.1007/s003480000232
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Experiments are performed to study the characteristics of rectangular cavity flows. Mean and fluctuating surface pressures in a Mach 1.28 turbulent flow past rectangular cavities are obtained. The cavity length-to-depth ratio (L/D) is varied from 2.43 to 43.00, while the length-to-width ratio (L/W) is 0.5, 1.0 and 2.0. The three-dimensional effect is significant on the trailing edge vortex, which affects the peak pressure ahead of the rear face, pressure gradient and levels of pressure fluctuation near the trailing edge, particularly for closed and transitional cavity flows. L/W and Mach number are important for the definition of critical LID for the cavity flowfield models.
引用
收藏
页码:531 / 536
页数:6
相关论文
共 50 条
  • [31] CALCULATION OF THREE-DIMENSIONAL UNSTEADY TRANSONIC FLOWS PAST HELICOPTER BLADES.
    Chattot, J.J.
    NASA Technical Paper, 1980, (1721):
  • [33] THREE-DIMENSIONAL VISCOUS FLUTTER ANALYSES OF A TURBINE CASCADE IN SUBSONIC AND TRANSONIC FLOWS
    Micallef, Derek
    Witteck, Dirk
    Wiedermann, Alexander
    Kluss, David
    Mailach, Ronald
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 7, PTS A AND B, 2012, : 1441 - +
  • [34] Three-dimensional simulation of Rayleigh-Benard convection in a rectangular cavity
    Zhan, N. Y.
    Yang, M.
    Wang, Z. Y.
    Li, L.
    Zheng, Z. Z.
    PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2008, 8 (7-8): : 526 - 535
  • [35] Three-dimensional vortex dynamics in a shear-driven rectangular cavity
    Chiang, TP
    Sheu, WH
    Hwang, RR
    INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 1997, 8 (03) : 201 - 214
  • [36] Two-dimensional and three-dimensional cavity flows at hypersonic speeds.
    Jackson, A
    Soltani, S
    Hillier, R
    PROCEEDINGS OF THE THIRD EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES, 1999, 420 : 283 - 289
  • [37] Three-dimensional transonic shocks in a nozzle
    Xin, Zhouping
    Yin, Huicheng
    PACIFIC JOURNAL OF MATHEMATICS, 2008, 236 (01) : 135 - 193
  • [38] Calculation of three-dimensional transonic flows in turbomachinery with generalized von Mises corrdinate system
    沈孟育
    刘秋生
    张增产
    Science China Mathematics, 1996, (10) : 1084 - 1095
  • [39] Calculation of three-dimensional transonic flows in turbomachinery with generalized von Mises corrdinate system
    沈孟育
    刘秋生
    张增产
    ScienceinChina,SerA., 1996, Ser.A.1996 (10) : 1084 - 1095
  • [40] Calculation of three-dimensional transonic flows in turbomachinery with generalized von Mises coordinate system
    Shen, MY
    Liu, QS
    Zhang, ZC
    SCIENCE IN CHINA SERIES A-MATHEMATICS PHYSICS ASTRONOMY, 1996, 39 (10): : 1084 - 1095