Viscous and inviscid linear/nonlinear calculations versus quasi-three-dimensional experimental cascade data for a new aeroelastic turbine standard configuration

Journal of Turbomachinery

Volumn 121, Issue 4, 1999, Pages 717-725

  Fransson, T H ^a   Jocker M ^a   Boles A ^b   Ott, P ^b  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b EPFL   (Switzerland)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; BLADE; MATHEMATICAL ANALYSIS; NAVIER-STOKES EQUATIONS; TURBINE;

EID: 0343415685     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2836725     Document Type: Article

References (36)

1. Anderson, W. K., Thomas, J. L., and van Leer, B., 1987, “A Comparison of Finite Volume Flow with Shock Waves,” AIAA Paper No. 87-1152.
2. Baldwin, B., and Lomax, L., 1978, “Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow,” AIAA Paper No. 78-257; 197883.
3. Beam, R. M., and Warming, R. F., 1977, “An Implicit Factored Scheme for the Compressible Navier-Stokes Equations,” Proc. 3rd Computational Fluid Dynamics Conference, Albuquerque, NM.
4. Boles, A., and Körbächer, H., 1993, “Periodicity and Repetivity of Unsteady Measurements of an Annular Turbine Cascade at Off-Design Flow Conditions,” ASME Paper No. 93-GT-107.
5. Bölcs, A., Fransson, T. H., and Körbächer, H., 1991, “Time-Dependent Pressure Fluctuations on an Oscillating Turbine Cascade at Transonic Off-Design Flow Conditions,” in: Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines and Propellers, H. M. Atassi, ed., Springer-Verlag, New York, pp. 547-565.
6. Bölcs, A., Fransson, T. H., and Platzer, M. F., 1989, “Numerical Simulation of Inviscid Transonic Flow Through Nozzels With Fluctuating Back Pressure,” ASME Journal of Turbomachinery, Vol. Ill, pp. 169-180.
7. Bölcs, A., and Fransson, T. H., 1986, “Aeroelasticity in Turbomachines, Comparison of Theoretical and Experimental Cascade Results,” Communication de Laboratoire de Thermique Apliquee et de Turbomachines, No. 1, EPF Lausanne, Switzerland.
8. Bölcs, A., 1983, “A Test Facility for the Investigation of Steady and Unsteady Transonic Flows in Annular Cascades," ASME Paper No. 83-GT-34.
9. Carstens, V., Bölcs, A., and Körbächer, H., 1993, “Comparison of Experimental and Theoretical Results for Unsteady Transonic Cascade Flow at Design and OffDesign Conditions,” ASME Paper No. 93-GT-100.
10. Fransson, T. H., and Verdon, J. M., 1991, “Updated Report on Standard Configurations for Unsteady Flow Through Vibrating Axial-Flow Turbomachine Cascades,” Report Royal Institute of Technology, Stockholm, Sweden; available on internet via http://www.egi.kth.se/ekv/stcf.
11. Fransson, T. H., and Verdon, J. M., 1991, “Standard Configurations for Unsteady Flow Through Vibrating Axial-Flow Turbomachine Cascades,” in: Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines and Propellers, H. M. Atassi, ed., Springer-Verlag, New York, pp. 859-889.
12. Fransson, T. H., and Pandolfi, M., 1986, “Numerical Investigation of Unsteady Subsonic Compressible Flows Through an Oscillating Cascade,” ASME Paper No. 86-GT-304.
13. Gerolymos, G. A., and Vallet, I., 1996, “Validation of 3D Euler Methods for Vibrating Cascade Aerodynamics,” ASME Journal of Turbomachinery, Vol. 118, pp. 771-782.
14. Giles, M. B., 1989, “Non-reflecting Boundary Conditions for Euler Equation Calculations,” AIAA Journal, Vol. 28, No. 12, pp. 2050-2058.
15. Giles, M., and Heimes, R., 1993, “Validation of a Numerical Method for Unsteady Flow Calculations,” ASME Journal of Turbomachinery, Vol. 115, pp. 110-117.
16. Griiber, B., and Carstens, V., 1998, “Computation of the Unsteady Transonic Flow in Harmonically Oscillating Turbine Cascades Taking Into Account Viscous Effects,” ASME Journal of Turbomachinery, Vol. 120, pp. 104-111.
17. Groth, J. P., Mártensson, H., and Eriksson, L. E., 1996, “Validation of a 4D Finite Volume Method for Blade Flutter,” ASME Paper No. 96-GT-429.
18. Hall, K. C., and Crawley, E. F., 1989, “Calculation of Unsteady Flows in Turbomachinery Using the Linearized Euler Equations,” AIAA J., Vol. 27, pp. 778-787.
19. He, L., 1990, “An Euler Solution for Unsteady Flows Around Oscillating Blades,” ASME Journal of Turbomachinery, Vol. 112, pp. 714-722.
20. Holmes, D. G., and Chuang, H. A., 1991, “2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response,” in: Unsteady Aerodynamics, Aeroacous-tics and Aeroelasticity of Turbomachines and Propellers, H. M. Atassi, ed., SpringerVerlag, New York, pp. 213-230.
21. Huff, D. L., 1991, “Unsteady Flow Field Predictions for Oscillating Cascades,” in: Unsteady Aerodynamics, Aeroacoitstics and Aeroelasticity of Turbomachines and Propellers, H. M. Atassi, ed., Springer-Verlag, New York, pp. 127-148.
22. Imfeld, L., 1997, “Numerical Determination of Unsteady Flow Through Vibrating Turbomachine-Cascades: International Standard Configurations 4 and 11 with the NOVAC2D60 Code,” Diploma Thesis, KTH Stockholm.
23. Jocker, M., 1994, “Validation of Unsteady Aerodynamic Prediction Models on the Turbine Configuration TCT III,” Project Study, KTH Stockholm.
24. Kahl, G., and Klose, A., 1991, “Time Linearized Euler Calculations for Unsteady Quasi-3D Cascade Flows,” in: Unsteady Aerodynamics, Aeroacoitstics and Aeroelasticity’ of Turbomachines and Propellers, H. M. Atassi, ed., Springer-Verlag, New York, pp. 109-126.
25. Krainer, A., Hambraeus, T., and Fransson, T. H., 1998, “Highly Nonreflecting Boundary Conditions for Nonlinear Euler Calculations of Unsteady Turbomachinery Flows,” submitted to AIAA Journal of Propulsion and Power.
26. Leyland, P., Ott, P., and Richter, R., 1994, “Turbine Cascade Calculations With Structured and Unstructured Meshes,” presented at Second Computational Fluid Dynamics Conference, ECCOMAS, Stuttgart.
27. Norryd, M., and Boles, A., 1997, “Experimental Investigation Regarding Evolution of Unsteady Pressure in a Vibrating Turbine Cascade With Tip Gap Effects,” presented at the 8th International Symposium on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Stockholm.
28. Ott, P., Norryd, M., and Boles, A., 1998, “The Influence of Tailbords on Unsteady Measurements in a Linear Cascade,” ASME Paper No. 98-GT-572.
29. Ott, A., Boles, A., and Fransson, T. H., 1995, “Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle,” ASME Journal of Turbomachinery, Vol. 117, pp. 106-114.
30. Rolls-Royce, 1989, “FINSUP User Guide and Reference Manual, Issue 2,” RollsRoyce Commercial Technology; Rolls Royce pc., England.
31. Sidén, G., 1991, “Numerical Solution of Viscous Compressible Flows Applied to Turbomachinery Blade Flutter,” Ph. D. Thesis, Chalmers University of Technology, Goteborg.
32. Smith, T. E., 1989, “A Modal Aeroelastic Analysis Scheme for Turbomachinery Blading,” NASA Report CR-187089.
33. Smith, S. N., 1972, “Discrete Frequency Sound Generation in Axial Flow Turbomachines,” Reports and Memoranda No. 3709, Cambridge.
34. Verdón, J. M., and Caspar, J. K., 1984, “A Linear Aerodynamic Analysis for Unsteady Transonic Cascades,” NASA-CR, 3833.
35. Whitehead, D. S., 1990, “A Finite Element Solution of Unsteady TwoDimensional Flow in Cascades,” International Journal of Numerical Methods in Fluids, Vol. 10.
36. Whitehead, D. S., and Newton, S. G., 1985, “A Finite Element Solution of Unsteady Two-Dimensional Transonic Flows in Cascades,” International Journal of Numerical Methods in Fluids, Vol. 5, pp. 115-132.