On modeling of transitional flow and its application on a high lift multi-element airfoil configuration

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Krumbein, Andreas ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING;

INTERMITTENCY FUNCTION; LAMINAR SEPARATION POINTS; LAMINAR SEPARATIONS; MULTI ELEMENT AIRFOILS; TRANSITION LENGTH; TRANSITION LOCATIONS; TRANSITION PREDICTION; TRANSITIONAL FLOW;

TRANSITION FLOW;

EID: 85086614602     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/1.139     Document Type: Conference Paper

References (17)

1. Radespiel, R.; Graage, K.; Brodersen, O.: "Transition Predictions Using Reynolds-Averaged Navier-Stokes and Linear Stability Analysis Methods, " AIAA 91-1641, 1991.
2. Smith, A. M. O.; Gamberoni, N.: "Transition, Pressure Gradient and Stability Theory, " Douglas Aircraft Company, Long Beach, Calif. Rep. ES 26388, 1956.
3. van Ingen, J. L.: "A suggested Semi-Empirical Method for the Calcula-tion of the Boundary Layer Transition Region, " Univ. of Delft, Dept. Aerosp. Eng., Delft, The Netherlands, Rep. VTH-74, 1956.
4. Stock, H. W.; Haase, W.: "A Feasibility Study of eN Transition Prediction in Navier-Stokes Methods for Airfoils, " AIAA Journal, Vol. 37, no. 10, pp. 1187-1196, 1999.
5. Horton, H. P.; Stock, H. W.: "Computation of Compressible, Laminar Boundary Layers on Swept, Tapered Wings, " J. Aircraft, Vol. 32, pp. 1402-1405, 1995.
6. Stock, H. W.; Degenhardt, E.: "A simplified eN method for transition prediction in two-dimensional, incompressible boundary layers, " Z. Flugwiss. Weltraumforsch., Vol. 13, pp. 16-30, 1989.
7. Warren, E. S.; Hassan, H. A.: "Transition Closure Model for Predicting Transition Onset, " J. Aircraft, Vol. 35, pp. 769-775, 1998.
8. Czerwiec, R. M.; Edwards, J. R.; Rumsey, C. L.; Bertelrud, A.; Hassan, H. A.: "Study of High-Lift Configurations Using k-z Transition/Turbulence Model, " AIAA 99-3186, 1999.
9. Edwards, J. R.; Roy, C. J.; Blottner, F. G.; Hassan, H. A.: "Development of a One-Equation Transition/Turbulence Model, " AIAA Journal, Vol. 39, no. 9, pp. 1691-1698, 2001.
10. FLOWer-Installation and User Handbook, Release 116, Doc. Nr. MEGAFLOW-1001, Institut für Entwurfsaerodynamik, Deutsches Zentrum für Luft-und Raumfahrt e. V., 2000.
11. Krumbein, A.; Stock, H. W.: "Laminar-turbulent Transition Modeling in Navier-Stokes Solvers using Engineering Methods, " ECCOMAS 2000, Barcelona (e), 11.-14. September 2000, ECCOMAS 2000-CDRom Proceedings, Hrsg.: International Center for Numerical Methods in Engineering (CIMNE), 2000, ISBN: 84-89925-70-4, Depósito Legal: B-37139-2000.
12. Krumbein, A.: "Coupling of the DLR Navier-Stokes Solver FLOWer with an eN-Database Method for laminar-turbulent Transition Prediction on Airfoils, " Notes on Numerical Fluid Mechanics-Vol. 77, pp. 92-99, Springer Verlag, 2002.
13. Stock, H. W.; Haase, W.: "Navier-Stokes Airfoil Computations with eN Transition Prediction Including Transitional Flow Regions, " AIAA Journal, Vol. 38, no. 11, pp. 2059-2066, 2000.
14. High Level Modelling of High Lift Aerodynamics-HiAer, Annex 1, "Description of Work, " GROWTH Project GRD1-2000-25226 HiAer.
15. Dhawan, S.; Narasimha, R.: "Some properties of boundary layer flow during the transition from laminar to turbulent motion, " Journal of Fluid Mechanics, Vol. 3, pp. 418-436, 1958.
16. Walker, G. J.: " Transitional Flow on Axial Turbomachine Blading, " AIAA Journal, Vol. 27, No. 5, pp. 595-602, 1989.
17. Brodersen, O.; Ronzheimer, A.; Ziegler, R.; Kunert, T.; Wild, J.; Hepperle, M.: "Aerodynamic Applications using MegaCads, " Proc. of 6th International Conference on Numerical Grid Generation in Computational Field Simulation, editor: M. Cross, publisher: ISGG, NSF Eng. Research Center, Mississippi State University, pp. 793-802, 1998.