Detached-eddy simulation with compressibility corrections applied to a supersonic axisymmetric base flow
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[1] Stephen B. Pope,et al. The calculation of near-wake flows , 1976, Journal of Fluid Mechanics.
[2] M. W. Rubesin. Compressibility effects in turbulence modeling , 1982 .
[3] L. E. Putnam,et al. Results of AGARD assessment of prediction capabilities for nozzle afterbody flows , 1985 .
[4] H. Petrie,et al. Comparison of experiment and computation for a missile base region flowfield with a centered propulsive jet , 1985 .
[5] Steven C. Caruso,et al. On the Accuracy of Turbulent Base Flow Predictions , 1987 .
[6] Aspects of grid topology for Reynolds-averaged Navier-Stokes base flow computations , 1988 .
[7] Clinton P. T. Groth,et al. Assessment of Riemann solvers for unsteady one-dimensional inviscid flows for perfect gases , 1988 .
[8] Robert E. Childs,et al. Assessment of modeling and discretization accuracy for high speed afterbody flows , 1989 .
[9] Steven C. Caruso,et al. Assessment of modeling and discretization accuracy for high-speed afterbody flows , 1991 .
[10] S. Goebel,et al. EXPERIMENTAL STUDY OF COMPRESSIBLE TURBULENT MIXING LAYERS , 1991 .
[11] A. J. Peace,et al. Turbulent flow predictions for afterbody/nozzle geometries includingbase effects , 1989 .
[12] Noel T. Clemens,et al. Two- and three-dimensional effects in the supersonic mixing layer , 1990 .
[13] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .
[14] F. R. Menter,et al. Influence of freestream values on k-omega turbulence model predictions , 1992 .
[15] F. Menter. Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .
[16] F. Menter. ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .
[17] D. Wilcox. Turbulence modeling for CFD , 1993 .
[18] J. C. Dutton,et al. Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody , 1993 .
[19] Wei Shyy,et al. A numerical analysis of supersonic flow over an axisymmetric afterbody , 1993 .
[20] F. Menter. Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .
[21] Jubaraj Sahu,et al. Numerical Computations of Supersonic Base Flow with Special Emphasis on Turbulence Modeling , 1994 .
[22] J. C. Dutton,et al. Recent progress on high-speed separated base flows , 1995 .
[23] Russell M. Cummings,et al. Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies , 1995 .
[24] Michael S. Shur,et al. Comparative numerical testing of one- and two-equation turbulence models for flows with separation and reattachment , 1995 .
[25] Tarun Mathur,et al. BASE-BLEED EXPERIMENTS WITH A CYLINDRICAL AFTERBODY IN SUPERSONIC FLOW , 1996 .
[26] Shahyar Pirzadeh,et al. Three-dimensional unstructured viscous grids by the advancing-layers method , 1996 .
[27] Ching-Chang Chieng,et al. Supersonic base-flow computation using higher-order closure turbulence models , 1996 .
[28] George Karypis,et al. Parmetis parallel graph partitioning and sparse matrix ordering library , 1997 .
[29] Lakshmi N. Sankar,et al. An implicit algorithm for solving time dependent flows on unstructured grids , 1997 .
[30] P. Spalart. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach , 1997 .
[31] Tarun Mathur,et al. Planar visualizations of large-scale turbulent structures in axisymmetric supersonic base flows , 1998 .
[32] Robert Tomaro,et al. Cobalt: a parallel, implicit, unstructured Euler/Navier-Stokes solver , 1998 .
[33] Vipin Kumar,et al. A Parallel Algorithm for Multilevel Graph Partitioning and Sparse Matrix Ordering , 1998, J. Parallel Distributed Comput..
[34] Yildirim Suzen,et al. Investigation of Supersonic Jet Exhaust Flow by One-and Two-Equation Turbulence Models , 1998 .
[35] P. Harris,et al. Numerical Investigation of the Unsteady Behavior of Supersonic Plane Wakes , 1998 .
[36] Robert Tomaro,et al. The defining methods of Cobalt-60 - A parallel, implicit, unstructured Euler/Navier-Stokes flow solver , 1999 .
[37] James R. Forsythe,et al. Investigation of modified Menter's two-equation turbulence models for supersonic applications , 1999 .
[38] James R. Forsythe,et al. Application of several turbulence models for high speed shear layer flows , 1999 .
[39] C. Fureby,et al. Large eddy simulation of supersonic base flow , 1999 .
[40] Philippe R. Spalart,et al. Detached-eddy simulation of an airfoil at high angle of attack , 1999 .
[41] Strategies for turbulence modelling and simulations , 2000 .
[42] William Z. Strang,et al. Validation of several Reynolds-averaged turbulence models in a 3-D unstructured grid code , 2000 .
[43] K. Squires,et al. LES and DES investigations of turbulent flow over a sphere , 2000 .
[44] John R. Chawner,et al. AIAA 2000-0679 Development and Implementation of Gridgen's Hyperbolic PDE and Extrusion Methods , 2000 .
[45] Philippe R. Spalart,et al. Detached-Eddy Simulations Past a Circular Cylinder , 2000 .
[46] James R. Forsythe,et al. Detached-eddy simulation of a supersonic axisymmetric base flow with an unstructured solver , 2000 .
[47] Philippe R. Spalart,et al. Trends in turbulence treatments , 2000 .
[48] M. Strelets. Detached eddy simulation of massively separated flows , 2001 .
[49] R Spalart Philippe,et al. Young-Person''s Guide to Detached-Eddy Simulation Grids , 2001 .
[50] Jack R. Edwards,et al. AN ASSESSMENT OF BOUNDARY TREATMENT AND ALGORITHM ISSUES ON HYBRID RANS/LES SOLUTION STRATEGIES , 2001 .
[51] James R. Forsythe,et al. Detached-Eddy Simulation with compressibility corrections applied to a supersonic axisymmetric base flow , 2002 .
[52] F. Menter. Influence of Freestream Values on ku Turbulence Model Predictions , 2003 .
[53] Florian,et al. Improved Two-Equation k- Turbulence Models for Aerodynamic Flows , 2022 .