Experimental and computational investigation of an 'open' transonic cavity flow

被引:21
|
作者
Atvars, K. [2 ]
Knowles, K. [2 ]
Ritchie, S. A. [2 ]
Lawson, N. J. [1 ]
机构
[1] Cranfield Univ, Natl Flying Lab Ctr, Cranfield MK43 0AL, Beds, England
[2] Cranfield Univ, Aeromech Syst Grp, Shrivenham, England
基金
英国工程与自然科学研究理事会;
关键词
transonic cavity; flow visualization; particle image velocimetry (PIV); unsteady Reynolds-averaged Navier-Stokes (URANS); CFD;
D O I
10.1243/09544100JAERO445
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents an investigation of a transonic flow (M-infinity = 0.85) over a rectangular cavity having a length-to-depth ratio of 5. Velocities were measured inside the cavity on the central plane and two off-centre planes using a two-component particle image velocimetry system. These measurements were supported by surface flow visualization, and mean and time-varying surface pressure measurements. The flow was also simulated using an unsteady Reynolds-averaged Navier-Stokes code, with a realizable kappa - epsilon turbulence model. It is shown that this CFD model does not capture all the characteristics of the flowfield correctly. However, by using this integrated experimental and computational approach we have been able to identify three-dimensional flowfield structures within the cavity. The influence of the thickness of the approaching boundary layer is discussed.
引用
收藏
页码:357 / 368
页数:12
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