UFR 2-05 References
Flow around airfoils (and blades) A-airfoil (Ma=0.15,
Re/m=2x106)
Underlying Flow Regime 2-05 © copyright ERCOFTAC 2004
References
1. EUROVAL: A European Initiative on Validation of CFD Codes. Notes on Numerical Fluid Mechanics 42. (ed. W. Haase, F. Brandsma, E. Elsholz, M. Leschziner and D. Schwamborn). Article 5.3 “Maximum Lift Investigations for A-Airfoil”, 269-282, by A. Kourta and F.J. Brandsma. Vieweg Verlag, 1993.
2. ECARP - European Computational Aerodynamics Research Project: Validation of CFD Codes and Assessment of Turbulence Models. Notes on Numerical Fluid Mechanics 58. (ed. W. Haase, E. Chaput, E. Elsholz, M. Leschziner and U. Müller) Vieweg Verlag 1997.
3. LESFOIL — Large Eddy Simulation of Flow around a High-Lift Aerofoil. (ed. L. Davidson, D. Cokljat, F. Frölich, M. Leschziner, C. Mellen and W. Rodi) Springer, 2003. (ISBN 3-540-00533-1)
4. A. Jirásek, P.Eliasson and S Wallin (2001a). “Computational Study of the High-Lift A-airfoil”. AIAA 2001-0708
5. A. Jirásek, P.Eliasson and S Wallin (2001b). “Computational Study of the High-Lift A-airfoil”. Engineering Notes, J. Aircraft, 38, 4, 769-772.
6. P. Capberne and Ch. Bonnet (1989) “Opération décrochage — Rapport final de synthèse” AEROSPATIALE TR 443.535/89.
7. Ch. Gleyzes (1988) “Opération décrochage — Résultats des essais à la soufflerie F2”, RT-DERAT 55/4004.
8. Ch. Gleyzes (1989) “Opération décrochage — Résultats de la 2me campagne d’essais à F2 — Mesures de pression et vélocimétrie laser”, RT-DERAT 55/5004.
9. A.M. Rodde (1987) “Opération décrochage — Exploitation des essais à la soufflerie F2 sur les profils A et B”, RSF No 74/1685 AYG, ONERA.
10. R. Houdeville, O. Piccin et D. Cassoudesalle (1987) “Opération décrochage — Mesures de frottements sur profils AS239 et AS240 à la soufflerie F1 du CFM”, RT-DERAT 19/5025 DN.
11. L. Lorenzen and I.A.A. Lindblad (1999). “Application of Two-Equation and EARSM Turbulence Models to High Lift Aerodynamics” AIAA 99-3181.
12. F. Lien and M. Leschziner (1995) “Modelling of 2D Separation from High-Lift Aerofoils with a Non-linear Eddy-viscosity Model and Second Moment Closure.” The Aeronautical Journal 99, 125-144.
13. L. Davidson and A. Rizzi (1992) “Navier-Stokes Stall Predictions Using an Algebraic Stress Model”. J. Spacecraft Rockets 29, 794-800.
© copyright ERCOFTAC 2004
Contributors: Peter Voke - University of Surrey