Sensitivity to Physical and Numerical Modeling in Navier-Stokes Simulations
Publication: Journal of Aerospace Engineering
Volume 13, Issue 2
Abstract
Navier-Stokes Multiblock code solves the fully coupled system of equations simultaneously using a cell-centered finite-volume approach. This note assesses the sensitivity to some turbulence models and numerical schemes implemented in Navier-Stokes Multiblock when computing two test cases in standard mode, i.e., without tuning the code to these two cases. The cases are (1) subsonic flow around the MS(1)-0313 airfoil, and (2) transonic flow around the ONERA M6 wing, using various combinations of models (algebraic Baldwin-Lomax or Granville, one-equation Spalart-Allmaras, or the two-equation k − ε model of Chien) together with a numerical scheme of either the second-order central or third-order Roe upwind type.
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References
1.
Baldwin, B. S., and Lomax, H. (1978). “Thin layer approximation and algebraic model for separated turbulent flows.” AIAA Paper 78-257, American Institute of Aeronautics and Astronautics, Reston, Va.
2.
Cella, U. ( 1998). “Assessment of physical and numerical models in NSMB for flow around aerofoils and wings,” Master's thesis, Royal Institute of Technology (KTH), Stockholm, Sweden.
3.
Gacherieu, C., and Weber, C. (1998). “Assessment of algebraic and one-equation turbulence models for the transonic turbulent flow around a full aircraft configuration.” AIAA Paper No. 98-2737, American Inst. of Aeronautics and Astronautics, Reston, Va.
4.
McGhee, R. J., and Beasley, W. D. (1979). “Low-speed aerodynamic characteristics of a 13-percent-thick medium-speed airfoil designed for general aviation application.” Tech. Rep., NASA Langley Research Center, Hampton, Va.
5.
Muller, B., and Rizzi, A. ( 1990). “Modelling of turbulent transonic flow around aerofoils and wings.” Applied numerical methods, vol. 6, 603–613.
6.
Schmitt, V., and Charpin, F. (1979). “Pressure distribution on the onera m6 wing at transonic mach number.” Tech. Rep., Office National D'Etudes et de Recherches Aerospatiales, 92320 Chatillon, France.
7.
Schmitt, V., Destarac, D., and Chaumet, B. (1983). “Viscous effects on a swept wing in transonic flow.” AIAA Paper 83-1804, American Inst. of Aeronautics and Astronautics, Reston, Va.
8.
Spalart, P. R., and Allmaras, S. R. (1992). “A one-equation turbulence model for aerodynamic flows.” AIAA Paper 92-0439, American Inst. of Aeronautics and Astronautics, Reston, Va.
9.
Tulapurkara, E. G. (1997). “Turbulence models for the computation of flow past airplanes.” Prog. Aerosp. Sci., 33, 71–165.
10.
Vatsa, V. N. (1987). “Accurate numerical solution for transonic viscous flow over finite wings. J. Aircraft, 6, June, 973–980.
11.
Vos, J. B., et al. (1998). NSMB handbook. Ecole Polytechnique Federale de Lausanne, Lausanne, Switzerland.
12.
Vos, J. B., Rizzi, A., Corjon, A., Chaput, E., and Soinne, E. (1998). “Recent advances in aerodynamics inside the nsmb consortium.” AIAA Paper 98-0225, American Inst. of Aeronautics and Astronautics, Reston, Va.
13.
Yoon, S., and Jameson, A. (1987). “Lower-upper implicit schemes with multiple grids for the Euler equations.” AIAA J., 25(7), 929–935.
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Received: Apr 22, 1999
Published online: Apr 1, 2000
Published in print: Apr 2000
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