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Acknowledgments

The authors would like to thank the CEC (UNSI, 'Unsteady Viscous Flow in the Context of Fluid-Structure Interaction', Project Ref: BRPR-CT97-0583) and the Deutsche Forschungsgemeinschaft (DFG-SFB 557 'Beeinflussung komplexer turbulenter Scherströmungen') for partly funding this research work.

References

  1. Spalart, P.R. and Allmaras, S.R. "A one-equation turbulence model for aerodynamic flows. "AIAA Paper, 92-0439, 1992.
  2. Menter, F.R. "Eddy Viscosity Transport Equations and Their Relation to the Model. "ASME J. Fluids Eng. Vol. 119, p 876, 1997.
  3. Edwards, J.R. and Chandra, S. "Comparison of Eddy Viscosity-Transport Turbulence Models for Three-Dimensional, Shock-Separated Flowfields." AIAA Journal, Vol. 34, No. 4, pp. 756-763, 1996.
  4. Monsen, E., Franke, M., Rung, T., Aumann, P. and Ronzheimer, A. "Assessment of Advanced Transport-Equation Turbulence Models for Aircraft Aerodynamic Performance Prediction." AIAA Paper99--3701, 1999.
  5. Gendre, P. "Maximum lift for single--element airfoils." BRITE EURAM: EUROVAL Task 2.1. Experiments: CERFACS, France, 1990.
  6. Cook, P.H., McDonald, M.A. and Firmin, M.C.P. "Aerofoil 28222 - pressure distribution, boundary-layer and wake measurements." AGARD Report AR-138, NATO, 1979.
  7. Shur, M.L, Strelets, M., Travin, A.K. and Spalart, P.R. "Turbulence Modeling in Rotating and Curved Channels: Assessing the Spalart-Shur Correction." AIAA Journal Vol. 38, No. 5, pp. 784-792, 2000.
  8. Rung, T., Bunge, U., Schatz, M. and Thiele, F. "Restatement of the Spalart-Allmaras Eddy-Viscosity Model in a Strain-Adaptive Formulation." AIAA Journal Vol. 41, No. 7, pp. 1396-1399, 2003.



  9. Markus Schatz 2004-02-10