Separated flow transition under simulated low-pressure turbine airfoil conditions - Part 2: Turbulence spectra

Journal of Turbomachinery

Volumn 124, Issue 4, 2002, Pages 656-664

  Volino, Ralph J ^a  

^a ASME   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; BOUNDARY LAYER FLOW; COMPUTER SIMULATION; PRESSURE EFFECTS; REYNOLDS NUMBER; SHEAR STRESS; SPECTRUM ANALYSIS; TURBULENCE;

FREE-STREAM TURBULENCE;

TURBINES;

AEROFOIL; FLOW SEPARATION; LOW PRESSURE; TURBINE; TURBULENCE;

EID: 0036820842     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1506939     Document Type: Article

References (15)

1. Volino, R. J., 2002, "Separated Flow Transition Under Low Pressure Turbine Airfoil Conditions: Part 1 - Mean Flow and Turbulence Statistics," ASME J. Turbomach., 124, pp. 645-655.
2. Mayle, R. E., 1991, "The Role of Laminar-Turbulent Transition in Gas Turbine Engines," ASME J. Turbomach., 116, pp. 509-537.
3. Schlichting, H., 1979, Boundary Layer Theory, 7th ed., McGraw Hill, New York, NY.
4. Sohn, K. H., and Reshotko, E., 1991, "Experimental Study of Boundary Layer Transition with Elevated Freestream Turbulence on a Heated Flat Plate," NASA CR 187068.
5. Volino, R. J., 2002, "An Investigation of the Scales in Transitional Boundary Layers Under High Free-Stream Turbulence Conditions," ASME Paper GT-2002-30233.
6. Hughes, J. D., and Walker, G. J., 2001, "Natural Transition Phenomena on an Axial Compressor Blade," ASME J. Turbomach., 123, pp. 392-401.
7. Halstead, D. E., Wisler, D. C., Okiishi, T. H., Walker, G. J., Hodson, H. P., and Shin, H.-W., 1997, "Boundary Layer Development in Axial Compressors and Turbines: Part 3 of 4-LP Turbines," ASME J. Turbomach., 119, pp. 225-237.
8. Solomon, W. I., and Walker, G. J., 1995, "Incidence Effects on Wake-Induced Transition on an Axial Compressor Blade," Proc. 12th Int. Symposium on Air Breathing Engines, Melbourne, Australia, pp. 954-964.
9. Hatman, A., and Wang, T., 1999, "A Prediction Model for Separated Flow Transition." ASME J. Turbomach., 121, pp. 594-602.
10. Volino, R. J., and Hultgren, L. S., 2001, "Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions," ASME J. Turbomach., 123, pp. 189-197.
11. Lou, W., and Hourmouziadis, J., 2000, "Separation Bubbles Under Steady and Periodic-Unsteady Main Flow Conditions," ASME J. Turbomach., 122, pp. 634-643.
12. Ligrani, P. M., and Bradshaw, P., 1987, "Spatial Resolution and Measurement of Turbulence in the Viscous Sublayer Using Subminiature Hot-Wire Probes," Exp. Fluids, 5, pp. 407-417.
13. Ligrani, P. M., and Bradshaw, P., 1987, "Subminiature Hot-Wire Sensors: Development and Use," J. Phys. E, 20, pp. 323-332.
14. Ligrani, P. M., Westphal, R. V., and Lemos, F. R., 1989, "Fabrication and Testing of Subminiature Multi-Sensor Hot-Wire Probes," J. Phys. E, 22, pp. 262-268.
15. Walker, G. J., 1989, "Transitional Flow on Axial Turbomachine Blading," AIAA J., 27, pp. 595-602.