Abstract
The Reynolds averaged Navier Stokes equations have been numerically solved for the case of a turbulent horseshoe vortex flow around an endwall mounted cylinder. Two different models were used, one grid containing 265,320 mesh points, and then a larger grid with 442,200 points. The two solutions obtained are compared to each other and against the experimental setup of Eckerle and Langston1 for a turbulent endwall cylinder at Reynolds number 550,000 based on cylinder diameter. Comparisons between total pressure loss, endwall static pressures, and velocity vectors show good agreement for the smaller mesh over most of the compared flow field. For the larger mesh, the position and size of the horseshoe vortex indicate the solution has not fully converged. The reasons for the difficulty in getting the larger mesh solution to converge are discussed.
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References
W. A. Eckerle, L. S. Langston “Measurements of a Turbulent Horseshoe Vortex Formed Around a Cylinder,” NASA Contractor Report 3986, June 1986.
D. Kwak, J. L. C. Chang, S. P. Shanks, S. R. Chakravarthy, “An Incompressible Navier-Stokes Flow Solver in Three-Dimensional Curvilinear Coordinate System Using Primitive Variables,” AIAA Paper No. 84-0253, AIAA 22nd Aerospace Sciences Meeting, Reno, Nevada, January 9–12, 1984.
J. L. C. Chang, D. Kwak, “On the Method of Pseudo-Compressibilty for Numerically Solving Incompressible Flows,” AIAA Paper No. 84-0252, AIAA 22nd Aerospace Sciences Meeting, Reno, Nevada, January 9–12, 1984.
C. A. Wagner, “Computations of a Horseshoe Vortex Around an Endwall Mounted Cylinder,” Ph.D Thesis, University of Connecticut, Storrs, Connecticut (in preparation).
A. J. Chorin, “A Numerical Method for Solving Incompressible Viscous Flow Problems,” J. Comp. Phys., vol. 2, pp. 12–16, 1967.
A. J. Musker, “Explicit Expression for the Smooth Wall Velocity Distribution in a Turbulent Boundary Layer,”AIAA J., vol. 17, no. 6, June 1979.
H. McDonald, R. W. Fish, “Practical Calculations of Transitional Boundary Layer,” Int. J. Heat Mass Transfer, vol. 16, pp. 1729–1744, 1973.
W. R. Briley, R. C. Büggeln, H. McDonald, “Solution of the Three-Dimensional Navier-Stokes Equations for a Steady Laminar Horseshoe Vortex Flow,” AIAA Paper No. 85-1029-CP, AIAA 7th Computational Fluid Dynamics Conference, Cincinnati, Ohio, July 15–17, 1985.
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© 2011 Plenum Press, New York
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Wagner, C. (2011). Navier Stokes Computations of a Turbulent Horseshoe Vortex Around an Endwall Mounted Cylinder. In: Kane, J.H., Carlson, A.D., Cox, D.L. (eds) Solution of Superlarge Problems in Computational Mechanics. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-0535-4_12
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DOI: https://doi.org/10.1007/978-1-4613-0535-4_12
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