Experimental and numerical investigation of boundary-layer and wake development in a transonic turbine cascade

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Michelassi, V ^a,b   Rodi, W ^a   Giess P A ^c  

^a UNIVERSITY OF KARLSRUHE   (Germany)

^b UNIVERSITY OF FLORENCE   (Italy)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; FLOW SEPARATION; GAS TURBINES; NUMERICAL METHODS; PRESSURE; SUPERSONIC AIRCRAFT; TURBULENCE MODELS; WAKES;

EXPERIMENTAL AND NUMERICAL METHODS; NUMERICAL INVESTIGATIONS; PRESSURE PROFILES; SHOCK BOUNDARY-LAYER INTERACTIONS; TRAILING EDGES; TRANSITION MODEL; TRANSONIC TURBINE; TRANSONIC TURBINE CASCADE;

BOUNDARY LAYERS;

EID: 84973641628     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-483     Document Type: Conference Paper

References (27)

1. Abu-Ghannam, BJ., Shaw, R., 1980, "Natural Transition of Boundary Layers - The effects of Turbulence, Pressure Gradient, and Flow History", Journal of Mechanical Engineering Science, Vol.22, No.5, pp.213-228.
2. Amecke, J., Salmi, P., 1995, "Data Reduction of Wake Flow Measurements with Injection of an Other Gas", DLR-FB 95-32, DLR, Kohl, Germany.
3. Brininling, W., Quast, A., Dietrichs, H.-J., 1988, "Detection of Separation Bubbles by Infrared Images in Transonic Turbine Cascades", ASME paper 88-gt-33.
4. Cho, N.-H., Liu, X., Rodi, W., Slitinung, B., 1993, "Calculation of Wake-Induced Unsteady Flow in a Turbine Cascade", ASME Journal of Turbomachinery, October, Vol.115, pp. 675-686.
5. GieP, P.-A., 1994, "Grenzschichtmessungen auf der Schaufeloberflache bei transsonischer und inkompressibler Durchstramung ebener Turbinengitter", Report D3 223 - 96 A 08, Gottingen, Germany.
6. Heinemann, H.-J. 1983, "The Test Facility for Rectilinear Cascades (EGG) of the DFVLR", D3 222 - 83 A 14, DFVLR, GOttingen, Germany.
7. Kato, M., Launder, B.E., 1993, "The Modelling of Turbulent Flow wound Stationary and Vibrating Square Cylinders", Proceedings Ninth Symposium of "Turbulent Shear Flows", Kyoto, Japan, August 16-18.
8. Kost, F., 1993, "Llingswirbelentstehung in einem Turbinenlaufrad mit konischen Seitenwanden", DLR-FB 93-13, DLR, Köln, Germany.
9. Kost, F., 1994, "Messungen des Geschwindigkeitsfeldes mit dem L2F-Velocimeter bei transsonischer und inkompressibler Durchstromung ebenex Turbinengitter", Report 1B 223-96 A 09, DLR, Gottingen, Germany.
10. Kost, F., GieP, P.-A., 1995, "Incompressible and Transonic Turbine Wake Flow Influenced by Vortex shedding". VDI Berichte NR. 1186, pp. 63-77.
11. Kwon, O.K., Pletcher, R.H., 1982, "Prediction of subsonic separation bubbles on airfoils by viscous-inviscid interaction". Second Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Iowa State University, Ames, Iowa, USA.
12. Lakshminarayana B., 1991, "An Assessment of Computational Fluid Dynamic Techniques in the Analysis and Design of l'urbomachinery - The 1990 Freeman Scholar Lecture", ASME J. of Fluids Eng., Vol. 113, pp. 315-352.
13. Mayle, RE., 1991, "The Role of Laminar-Turbulent Transition in Gas Turbine Engines", ASME Journal of Turbomachinery, vol. 113, October, pp. 509-537.
14. Michelassi, V., 1994, "A pressure correction algorithm for all speed flows", Report No.718, Institute for Hydromechanik, University of Karlsruhe, Germany.
15. Michelassi, V., 1996, "Turbulence and Transition Modelling in Transonic Turbine Rows", Report No.728, Institute for Hydromechanik, University of Karlsruhe, Germany.
16. Michelassi, V., Martelli, F., (1993), "3-D Implicit Navier-Stokes Solver for Internal Turbulent Compressible Rows", Journal de Phys. III, France 3, pp. 223-235.
17. Michelassi, V., Papanicolaou, E., Theodoridis, G., 1995a, "A Comparison of Time Marching and Pressure Correction Algorithms for Transonic Turbine Blades", 1995 International Mechanics Engineering Congress and Exposition, November 12-17, San Francisco, California, USA.
18. Michelassi, V., Theodoridis, G., Papanicolaou, E., 1995b, "Low Speed Turbine Computation by Pressure Correction and Time Marching Methods", 1995 International Mechanics Engineering Congress and Exposition, November 12-17, San Francisco, California, USA.
19. Norris, L.H., Reynolds, W.C., 1975, "Turbulent Channel Flow with Moving Wavy Boundary", Rept. No. FM-10, Stanford University, Dept of Mech. Eng..
20. Papanicolaou, E., 1996, "Computation of Separated Flow Transition Using a Two-layer Model of Turbulence", Report No.773, Institute for Hydromechanllc, University of Karlsruhe, Germany.
21. Roth, W., Bonnin, J.-C., Buchal, T. (Ed.), 1995, Proceedings of ERCOFTAC Workshop on "Data Bases and Testing of Calculation Methods for Turbulent Flows", University of Karlsruhe, Karlsruhe, Germany, April 3-7.
22. Rodi, W., Mansour, N.N., Michelassi, V., "One-Equation Near-Wall Modelling with the Aid of Direct Simulation Data", ASME Journal of Fluids Engineering, vol.115, June 1993, pp.196-205.
23. Roth, W., Shonung, B., 1987, "Interaktives-Inverses Grenzschichtverfahren zur Berechnung von lokalen Abffiseblasen an Tttrbinenschaufeln", Z. Flugwiss. Weltraumforsch. 11, pp. 271-280.
24. Sevin, A.M., 1993, "Farther Progress in the Turbulence Modelling of By-Pass Transition", Proceedings 2-nd International Symposium on Engineering Turbulence Modelling and Measurements", May 31- June 2, Florence, Italy.
25. Schodl, R. A, 1980, "Laser-Two-Focus (L2F) Velocimeter for Automatic Flow Vector Measurements in Rotating Components of Turbomachines", J. Fluid Eng., vol. 102, pp. 412-419.
26. Wilcox, D.C., 1988, "Reassessment of the Scale-Determining Equation for Advanced Turbulence Models", AIAA Journal, Vol. 26, No.11, pp. 1299-1310.
27. Zhu, J., 1992, "An Introduction and Guide to the Computer Program FAST-3D", Report No. 691, Institute for Hydromechanilc, University of Karlsruhe.