Turbulence model upgrades for swirling flows

被引:0
作者
Chenoweth, J. D. [1 ]
York, B. [2 ]
Hosangadi, A. [2 ]
机构
[1] Combust Res & Flow Technol Inc, Huntsville, AL 35801 USA
[2] Combust Res & Flow Technol Inc, Pipersville, PA 18947 USA
来源
FEDSM 2007: PROCEEDINGS OF THE 5TH JOINT AMSE/JSME FLUIDS ENGINEERING SUMMER CONFERENCE VOL 1, PTS A AND B | 2007年
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T [工业技术];
学科分类号
08 ;
摘要
The ability to accurately model axisymmetric, turbulent swirling jet flows over a variety of inflow conditions is evaluated. The deficiency of the standard k-epsilon turbulence model in predicting mixing rates in flows with streamline curvature is well known. A relatively straightforward modification to this model is made based on a local value of the flux Richardson number which accounts for the azimuthal velocity and its variation. To evaluate the effectiveness of this modification two different experimental data sets are used to compare the computational results against. All calculations were performed using the structured. density based, CRAFT CFD (R) code utilizing a preconditioning methodology. Both cases have initial swirl distributions that are equivalent to a solid-body rotation profile, and have swirl numbers that are low enough to remain below the vortex breakdown regime. They also have non-swirling jet data available for the same geometries and operating conditions which allows the increased jet mixing rate of swirling jets over purely axial jets to be confirmed. All calculations showed a significant improvement of centerline velocity decay as well as downstream radial velocity profiles when the Richardson number correction was activated. For the case with turbulence data, the centerline decay of turbulent kinetic energy was also much improved. An important result that was discovered was the extreme sensitivity of the downstream evolution of the jet to the specification of the initial k and epsilon profiles, highlighting the critical need for a comprehensive experimental characterization of all flow properties at the jet exit.
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页码:1961 / 1968
页数:8
相关论文
共 11 条
[1]  
BULZAN DL, 1987, 25 AER SCI ME REN NV
[2]   THE APPLICATION OF PRECONDITIONING IN VISCOUS FLOWS [J].
CHOI, YH ;
MERKLE, CL .
JOURNAL OF COMPUTATIONAL PHYSICS, 1993, 105 (02) :207-223
[3]   VISCOUS INVISCID ANALYSIS OF CURVED SUBSONIC OR SUPERSONIC WALL JETS [J].
DASH, SM ;
BEDDINI, RA ;
WOLF, DE ;
SINHA, N .
AIAA JOURNAL, 1985, 23 (01) :12-13
[4]   EFFECT OF INITIAL SWIRL DISTRIBUTION ON THE EVOLUTION OF A TURBULENT JET [J].
FAROKHI, S ;
TAGHAVI, R ;
RICE, EJ .
AIAA JOURNAL, 1989, 27 (06) :700-706
[5]   ON EXPLICIT ALGEBRAIC STRESS MODELS FOR COMPLEX TURBULENT FLOWS [J].
GATSKI, TB ;
SPEZIALE, CG .
JOURNAL OF FLUID MECHANICS, 1993, 254 :59-78
[6]   PREDICTION OF LAMINARIZATION WITH A 2-EQUATION MODEL OF TURBULENCE [J].
JONES, WP ;
LAUNDER, BE .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1972, 15 (02) :301-+
[7]   COMPUTATION OF STRONGLY SWIRLING AXISYMMETRIC FREE JETS [J].
LESCHZINER, MA ;
RODI, W .
AIAA JOURNAL, 1984, 22 (12) :1742-1747
[8]   Assessment and modification of two-equation turbulence models [J].
Pajayakrit, P ;
Kind, RJ .
AIAA JOURNAL, 2000, 38 (06) :955-963
[9]  
Papp J. L., 2001, 39 AIAA AER SCI M EX
[10]   EXPLANATION OF TURBULENT ROUND-JET-PLANE-JET ANOMALY [J].
POPE, SB .
AIAA JOURNAL, 1978, 16 (03) :279-281