论文信息 - Reynolds-Averaged Navier–Stokes Simulations on NACA0012 and ONERA-M6 Wing with the ONERA elsA Solver

Reynolds-Averaged Navier–Stokes Simulations on NACA0012 and ONERA-M6 Wing with the ONERA elsA Solver

Results of the elsA software package, the ONERA multipurpose tool for applied aerodynamics and multiphysics, are presented for a well-known NACA0012 configuration proposed by the turbulence modeling resource website of NASA Langley Research Center and on the ONERA-M6 wing. ONERA proposed new computer-aided design models for the turbulence modeling resources to make ONERA-M6 a reference test case. Results and solver performance are presented and discussed.

[1] V. N. Vatsa,et al. Accurate numerical solutions for transonic viscous flow over finite wings , 1987 .

[2] V. Vatsa,et al. Prediction of separated transonic wing flows with a non-equilibrium algebraic model , 1989 .

[3] Brian R. Smith,et al. Description of a Website Resource for Turbulence Modeling Verification and Validation , 2010 .

[4] John C. Vassberg,et al. Development of a Common Research Model for Applied CFD Validation Studies , 2008 .

[5] P. Sagaut,et al. Large Eddy Simulation of Flow Around an Airfoil Near Stall , 2002 .

[6] M. Liou,et al. A New Flux Splitting Scheme , 1993 .

[7] Laurent Cambier,et al. The Onera elsA CFD software: input from research and feedback from industry , 2013 .

[8] V. Gleize,et al. Verification and validation of the Onera elsA flow solver on RANS benchmarks , 2014 .

[9] Rolf Radespiel,et al. An efficient cell-vertex multigrid scheme for the three-dimensional Navier-Stokes equations , 1989 .

[10] C. L. Ladson,et al. Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section , 1988 .

[11] V. Vatsa,et al. Comparison of the predictive capabilities of several turbulence models , 1995 .

[12] Georg May,et al. Unstructured Algorithms for Inviscid and Viscous Flows Embedded in a Unified Solver Architecture: Flo3xx , 2005 .