Application of a hybrid Navier-Stokes solver with automatic transition prediction

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2007, Pages 1356-1376

  Krumbein, Andreas ^a,d   Krimmelbein, Normann ^b   Schrauf, Géza ^c,d,e  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

^c AIRBUS OPERATIONS GMBH   (Germany)

^d AIAA   (United States)

^e Laminar Flow Expert   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; BOUNDARY LAYERS; COMPUTATIONAL METHODS; PROBLEM SOLVING; REYNOLDS NUMBER; TURBULENT FLOW;

LAMINAR-TURBULENT TRANSITION; LINEAR STABILITY CODE; N FACTOR APPROACH; TOLLMIEN-SCHLICHTING;

NAVIER STOKES EQUATIONS;

EID: 35648977054     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4284     Document Type: Conference Paper

References (51)

1. Rudnik, R., Ronzheimer, A., and Schenk, M., "Berechnung von zwei- und dreidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes Gleichungen", Jahrbuch 1996 - Bd. II der Deutschen Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V. (DGLR) - JT 96-104, Deutscher Luft- und Raumfahrtkongreß, DGLR-Jahrestagung Sep. 1996, Dresden, Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V. (DGLR), Godesberger Allee 70, D-53175 Bonn, Germany, 1996, pp. 717-726.
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 Calculation of the Boundary Layer Transition Region", University of Delft, Dept. of Aerospace Engineering, Delft, The Netherlands, Rep. VTH-74, 1956.
4. Arnal, D., Casalis, G., "Laminar-turbulent transition prediction in three-dimesnional flows", Progress in Aerospace Sciences, Vol. 36, 2000, pp. 173-191.
5. Radespiel, R., Graage, K., Brodersen, O., "Transition Predictions Using Reynolds-Averaged Navier-Stokes and Linear Stability Analysis Methods", AIAA Paper 91-1641, 1991.
6. N Transition Prediction in Navier-Stokes Methods for Airfoils", AIAA Journal, Vol. 37, no. 10, 1999, pp. 1187-1196.
7. Horton, H. P., Stock, H. W., "Computation of Compressible, Laminar Boundary Layers on Swept, Tapered Wings", Journal of Aircraft, Vol. 32, 1995, pp. 1402-1405.
8. N method for transition prediction in two-dimensional, incompressible boundary layers", Zeitung für Flugwissenschaft und Weltraumforschung, Vol. 13, 1989, pp. 16-30.
9. Casalis, G., Arnal, D., "ELFIN II Subtask 2.3: Database method - Development and validation of the simplified method for pure crossflow instability at low speed", ELFIN II - European Laminar Flow Investigation, Technical Report no 145, ONERA-CERT, Département d'Études et de Recherches en Aérothermodynamique (DERAT), R.T. DERAT n° 119/5618.16, December 1996.
10. Crouch, J. D., Crouch, I. W. M., Ng, L. L., "Transition Prediction for Three-Dimensional Boundary Layers in Computational Fluid Dynamics Applications", AIAA Journal, Vol. 40, no. 8, 2002, pp. 1536-1541.
11. Warren, E. S., Hassan, H. A., "Transition Closure Model for Predicting Transition Onset", Journal of Aircraft, Vol. 35, 1998, pp. 769-775.
12. Czerwiec, R.M., Edwards, J. R., Rumsey, C. L., Bertelrud, A., Hassan, H. A., "Study of High-Lift Configurations Using k-ω Transition/ Turbulence Model", AIAA Paper 99-3186, 1999.
13. 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, 2001, pp. 1691-1698.
14. Langtry, R.B., Menter, F.R., "Transition Modeling for General CFD Applications in Aeronautics", AIAA Paper 2004-522, 2005.
15. Radespiel, R., Windte, J., Scholz, U., "Numerical and Experimental Analysis of Moving Airfoils with Laminar Separation Bubbles", AIAA Paper 2006-0501, 2006.
16. Windte, J., Scholz, U., Radespiel, R., "Validation of the RANS-Simulation of Laminar Separation Bubbles on Airfoils", Aerospace Science and Technology, Vol. 10, No. 6, 2006, pp. 484-494.
17. Wokoeck, R., Krimmelbein, N., Ortmanns, J., Ciobaca, V., Radespiel, R., Krumbein, A., "RANS Simulation and Experiments on the Stall Behaviour of an Airfoil with Laminar Separation Bubbles", AIAA Paper 2006-244, 2006.
18. Krumbein, A., Krimmelbein, N., "Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code", 15. DGLR-Fach-Symposium der STAB, Technical University of Darmstadt, Germany, 29 November - 1 December 2006, accepted for publication in New Results in Numerical and Experimental Fluid Mechanics, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Springer Verlag, Berlin.
19. Krumbein, A., "Automatic Transition Prediction and Application to High-Lift Multi-Element Configurations", Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 1150-1164;
20. also: AIAA Paper 2004-2543, June/July 2004.
21. Krumbein, A., "Automatic Transition Prediction and Application to Three-Dimensional Wing Configurations", Journal of Aircraft, Vol. 44, No. 1, 2007, pp. 119-133;
22. also: AIAA Paper 2006-914, January 2006.
23. Krumbein, A., "Automatic Transition Prediction and Application to 3-D High-Lift Configurations", in print at Journal of Aircraft, DOI: 10.2514/1.25528;
24. also: AIAA-2006-3164, June 2006.
25. N Transition Prediction in Three-Dimensional Boundary Layers on Inclined Prolate Spheroids", AIAA Journal, Vol. 44, No. 1, 2006, pp. 108-118.
26. Arthur, M.T., Atkin, C. J., "Transition modelling for viscous flow prediction", AIAA Paper 2006-3052, 2006.
27. Krimmelbein, N., Radespiel, R., Nebel, C., "Numerical Aspects of Transition Prediction for Three-Dimensional Configurations", AIAA-2005-4764.
28. TAU-Code User Guide, Release 2007.1.0, Institute of Aerodynamics and Flow Technology, German Aerospace Center, April 2007.
29. Schwamborn, D., Gerhold, T., Hannemann, V., "On the Validation of the DLR-TAU Code", New Results in Numerical and Experimental Fluid Mechanics II, Notes on Numerical Fluid Mechanics, Vol. 72, Braunschweig, Wiesbaden, Vieweg Verlag, 1999, pp. 426-433.
30. Kroll, N., Rossow, C-C, Schwamborn, D., Becker, K., and Heller, G., "MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design", ICAS Congress 2002 [CD-Rom], ICAS, Toronto, Canada, 2002, pp. 1.105.1-1.105.20.
31. Schwamborn, D., Gerhold, T., Heinrich, R., "The DLR TAU-Code: Recent Applications in Research and Industry", European Conference on Computational Fluid Dynamics, ECCOMAS CFD 2006, Egmond aan Zee, The Netherlands, 5 - 8 September 2006, ECCOMAS CFD 2006 - CD-Rom Proceedings, editors: P. Wesseling, E. Oñate, J. Périaux, 2006, ISBN: 90-9020970-0, ©TU Delft, The Netherlands.
32. Nebel, C., Radespiel, R., and Wolf, T., "Transition Prediction for 3D Flows Using a Reynolds-Averaged Navier-Stokes Code and N-Factor Methods", AIAA-2003-3593.
33. Krimmelbein, N., Radespiel, R., "Transition prediction for three-dimensional flows using parallel computation", submitted to Computers & Fluids, Elsevier, March 2007.
34. "COCO - A Program to compute Velocity and Temperature Profiles for Local and Nonlocal Stability Analysis of Compressible, Conical Boundary Layers with Suction", ZARM Technik Report, November 1998.
35. Schrauf, G., "LILO 2.1 User's Guide and Tutorial", Bremen, Germany, GSSC Technical Report 6, originally issued Sep. 2004, modified for Version 2.1 July 2006.
36. Rozendaal, R. A., "Natural Laminar Flow Flight Experiments on a Swept Wing Business Jet-Boundary-Layer Stability Analysis", NASA CP 3975, March 1986.
37. Rozendaal, R. A., "Variable-Sweep Transition Flight Experiment (VSTFE)-Parametric Pressure Distribution Boundary-Layer Stability Study and Wing Glove Design Task", NASA CR 3992, December 1986.
38. Rozendaal, R. A., "Variable-Sweep Transition Flight Experiment (VSTFE)-Stability Code Development and Clean-Up Glove Analysis", NASA CP 2847, April 1987.
39. Schrauf, G., "Large-Scale Laminar-Flow Tests Evaluated with Linear Stability Theory", Journal of Aircraft, Vol. 41, No. 2, March/April 2004, pp. 224 - 230.
40. N Transition Prediction - Feasibility Study", Rept. IB 124-2003/12, Deutsches Zentrum für Luft- und Raumfahrt (DLR), Braunschweig, Germany, Aug. 2002.
41. Krumbein, A., "Navier-Stokes Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code - A Sensitivity Study", New Results in Numerical and Experimental Fluid Mechanics 5, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 92, Springer Verlag, Berlin, 2006, pp. 192-199.
42. Krumbein, A., "Automatic Transition Prediction for High-Lift Systems Using a Hybrid Flow Solver", Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 1362-1366.
43. Schmidt, G. S., Mueller, Th. J., "Analysis of Low Reynolds Number Separation Bubbles Using Semiempirical Methods", AIAA Journal, Vol. 27, No. 8, 1989, pp. 993-1001.
44. Davis, R. L., Carter, J. E., Reshotko, E., "Analysis of Transitional Separation Bubbles on Infinite Swept Wings", AIAA Journal, Vol. 25, No. 3, March 1987, pp. 421-428.
45. Stock, H. W., Haase, W., "Some Aspects of Linear Stability Calculations in Industrial Applications", Transitional Boundary Layers in Aeronautics, Proceedings of the colloquium 'Transitional Boundary Layers in Aeronautics', Amsterdam, 6-8 December 1995, editors: Henkes, R. A. W. M.; van Ingen, J.L., Royal Netherlands Academy of Arts and Sciences, P.O. Box 1912, 1000 GC Amsterdam, The Netherlands, North-Holland, Amsterdam/Oxford/New-York/ Tokyo, ISBN: 0-444-85812-1, 1996, pp. 225-238.
46. van den Berg, B., "Boundary Layer Measurements on a Two-Dimensional Wing with Flap", National Aerospace Laboratory - NLR, Amsterdam, The Netherlands, NLR TR 79009 U, January 1979.
47. Spalart, P. R., and Allmaras, S. R., "A one-equation turbulence model for aerodynamic flows", La Recherche Aérospatiale, 1994, no 1, pp. 5-21.
48. 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, 1996, pp. 756-763.
49. N Transition Prediction for 3D Wing Configurations using Database Methods and a local, linear Stability Code", 7th ONERA-DLR Aerospace Symposium - ODAS 2006, 4-7 October 2006, Toulouse, France, ODAS 2006 - CD-ROM Proceedings, editor: ONERA, Centre de Toulouse, October 2006 (submitted to Aerospace Science and Technology).
50. Schrauf, G., Perraud, J., Lam, F., "Comparison of Boundary-Layer Transition Predictions Using Flight Test Data", Journal of Aircraft, Vol. 35, No. 6, 1998, pp. 891-897.
51. Schrauf, G., Atkin, Ch., "Progress in Linear Stability Methods for Design Applications", ECCOMAS 2000, Barcelona (e), 11.-14. September 2000, ECCOMAS 2000 - CD-Rom Proceedings, editor: International Center for Numerical Methods in Engineering (CIMNE), 2000, ISBN: 84-89925-70-4, Depósito Legal: B-37139-2000.