Numerical investigation of transitional flow over a rapidly pitching plate

被引:53
作者
Garmann, Daniel J. [1 ]
Visbal, Miguel R. [1 ]
机构
[1] USAF, Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
aerodynamics; boundary layer turbulence; external flows; flow simulation; laminar to turbulent transitions; numerical analysis; plates (structures); vortices; FINITE-DIFFERENCE SCHEMES; SIMULATION;
D O I
10.1063/1.3626407
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A computational study of a plate undergoing high amplitude, pitch, hold, and return motions is presented. An implicit large eddy simulation (ILES) technique is employed to capture the laminar-to-turbulent transition process as the plate is pitched to high angles of attack. Simulations are performed for Reynolds numbers between 5000 and 40 000 with motion profiles of varying accelerations and hold times. The solutions show extremely favorable flow field comparisons of span-averaged stream-wise velocity and out-of-plane vorticity with available experimental Particle Image Velocimetry (PIV) measurements. At a given Reynolds number, the span-averaged flow fields and aerodynamic loading show little sensitivity to the acceleration of the plate for the motions examined. The three-dimensional flow field structure reveals a very rapid transition process that occurs almost at the onset of motion for the higher Reynolds number cases. In spite of this, the aerodynamic loads for those cases compare closely with the same motions at lower Reynolds numbers. [doi: 10.1063/1.3626407]
引用
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页数:15
相关论文
共 39 条
[1]   IMPLICIT FILTERING IN CONJUNCTION WITH EXPLICIT FILTERING [J].
ALPERT, P .
JOURNAL OF COMPUTATIONAL PHYSICS, 1981, 44 (01) :212-219
[2]  
[Anonymous], 1981, 19811259 AIAA
[3]  
[Anonymous], 20012709 AIAA
[4]  
[Anonymous], 20101085 AIAA
[5]   IMPLICIT FACTORED SCHEME FOR COMPRESSIBLE NAVIER-STOKES EQUATIONS [J].
BEAM, RM ;
WARMING, RF .
AIAA JOURNAL, 1978, 16 (04) :393-402
[6]   PROGRESS IN ANALYSIS AND PREDICTION OF DYNAMIC STALL [J].
CARR, LW .
JOURNAL OF AIRCRAFT, 1988, 25 (01) :6-17
[7]   The leading-edge vortex and quasisteady vortex shedding on an accelerating plate [J].
Chen, Kevin K. ;
Colonius, Tim ;
Taira, Kunihiko .
PHYSICS OF FLUIDS, 2010, 22 (03) :1-11
[8]  
Ekaterinaris J., 1997, PROG AEROSP SCI, V14, P105
[9]  
Eldredge J.D., 2010, 20104281 AIAA
[10]  
Eldredge J.D., 2009, AIAA PAPER 2009 3687