Intermittent flow and thermal structures of accelerating transitional boundary layers, part 1: Mean quantities

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Wang, Ting ^a   Keller, F Jeffrey ^a,b  

^a Clemson University   (United States)

^b Accuracy Microsensers Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FRICTION; GAS TURBINES; REYNOLDS NUMBER; TURBULENT FLOW; WAKES;

ACCELERATION PARAMETERS; CONDITIONAL SAMPLING; LAMINAR TURBULENT TRANSITIONS; MEAN VELOCITY PROFILES; SKIN FRICTION COEFFICIENT; TRANSITIONAL BOUNDARY LAYERS; TURBULENT BOUNDARY LAYERS; ZERO PRESSURE GRADIENT;

LAMINAR BOUNDARY LAYER;

EID: 84973597737     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-402     Document Type: Conference Paper

References (28)

1. Blair, M.F., 1992, "Boundary-Layer Transition in Accelerating Flows with Intense Free-Stream Turbulence : Part 1- Disturbances Upstream of Transition Onset; Part 2-The Zone of Intermittent Turbulence, " ASME Journal of Fluids Engineering., Vol. 114, pp. 313-332.
2. Clauser, F.H., 1956, "The Turbulent Boundary Layer, " Advances in Applied Mechanics, Vol. 4, pp. 1-51.
3. Dey, J. and Narasimha, R., 1988, "An Integral Method for the Calculation of 2-0 Transitional Boundry Layers, " Fluid Mechanics Report 88 FM 7, Indian Institute of Science, Bangalore.
4. Dhawan, S. and Narasimha, R. 1958, "Some Properties of Boundary Layer Flow During the Transition From Laminar to Turbulent Flow, " Journal of Fluid Mechanics, Vol. 3, pp. 418-436.
5. Farmer, R. and Fulton, K., 1995, "Design 60% Net Efficiency in Frame 7/9 H Steam-Cooled CCGT, " Gas Turbine World, May- June, pp. 12-22.
6. Gostelow, J.P. and Blunden, A.R., 1988, "Investigations of Boundary Layer Transition in an Adverse Pressure Gradient, " ASME J. of Turbomacninery, Vol. 3, pp. 366-375.
7. Graham, R.W. 1979. "Fundamental Mechanisms That Influence the Estimate of Heat Transfer to Gas Turbine Blades, ASME paper" 79-HT-43, ASME, NASA TM-79128.
8. Graham, R.W. (editor), 1984, Transition in Turbines Symposium Proceedings, NASA CP-2386.
9. Halstead, D.E., Wisler, D.C., Okiishi, T.H., Walker, CJ., Hodson, H.P. and Shin, H., 1995, "Boundary Layer Development in Axial Compressor and Turbines, " Part 1: Composite Picture; Part 2: Compressors; Part 3: LP Turbines; Part 4: Computations and Analyses. ASME papers 95-GT-460, 461, 462, 463.
10. Hedley, T.B. and Keffer, IF., 1974, " Turbulent/Non- Turbulent Decisions in an Intermittent Row, " Journal of Fluid Mechanics, Vol. 64, pp. 625-644.
11. Keller, F.J., 1993, "Flow and Thermal Structures in Heated Transitional Boundary Layers with and without Streamwise Acceleration, " Ph.D. Dissertation, Department of Mechanical Engineering, Clemson University, Clemson, S.C.
12. Keller, F.J. and Wang, T. 1995, "Effects of Criterion Functions on Intermittency in Heated Transitional Boundary Layers with and Without Streamwise Acceleration, " ASME Journal of Turbomachinery, Vol. 117, pp. 154-165.
13. Keller, F.J. and Wang, T., 1996, "Flow and Thermal Behavior in Transitional Boundary Layers with Streamwise Acceleration." ASME Journal of Turbomachinery, Vol. 118, pp. 314-326.
14. Kim, J., Simon, T.W., and Kestoras, M. 1994, "Fluid Mechanics and Heat Transfer Measurements in Transitional Boundary Layers Conditionally Sampled on Intermittency, " ASME Journal of Turbomachinery, Vol. 116, pp.405-416.
15. Kuan, C.L. and Wang, T., 1990, "Investigation of the Intermittent Behavior of a Transitional Boundary Layer Using a Conditional Averaging Technique, " Experimental Thermal and Fluid Science, Vol. 3, pp. 157-170.
16. Launder, B.G., and Spalding, D.B., 1974 "The Numerical Computation of Turbulent Rows, " Computer Methods in Applied Mechanics and Engineering, Vol. 3. p 269.
17. Mayle, RE., 1991, "The Role of Laminar-Turbulent Transition in Gas Turbine Engines, " ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
18. Musker, A.J., 1979, "Explicit Expression for the Smooth Wall Velocity Distribution in Turbulent Boundary Layers, " AIAA Journal, Vol. 17, No. 6, June, pp. 655-657.
19. Narasimha, R. 1985, "The Laminar-Turbulent Transition Zone in a Boundary Layer, " Prog. Aero.Sci, Vol. 22, pp. 29-80.
20. Shome, B., 1991, "Development of a Three-Wire Probe for the Measurement of Reynolds Stresses and Heat Fluxes in Transitional Boundary Layers, " M.S. Thesis, Department of Mechanical Engineering, Clemson University, Clemson, S.C.
21. Sohn, K.H., O'Brien, J.E., and Reshotko, E., 1989. "Some Characteristics of Bypass Transition in a Heated Boundary Layer, " Proceeding of the 7th Turbulent Shear Flow Symposium, pp. 61- 70.
22. Sohn, KM. and Reshotko, E., 1991, "Experimental Study of Boundary Layer Transition with Elevated Free-Stream Turbulence on a Heated Plate, " NASA CR-187068.
23. Solomon, W. J., Walker, G. J., and Gostelow, J.-P., 1995, "Transition Length Prediction for Flows with Rapidly Changing Pressure Gradients, " ASME paper 95-GT-241.
24. Steelant, J. and Dick, E., 1996, "Modelling of Bypass Transition with Conditional Navier-Stokes Equations Coupled to an Intermittency Transport Equation." International Journal for Numerical Methods in Fluids, Vol. 23, pp. 193-220.
25. Turner, A.B., 1971, "Local Heat Transfer Measurements on a Gas Turbine Blade, " Journal of Mechanical Engineering Sciences, Vol. 13, 1, pp. 1-12.
26. Wang, T., Keller, F.J. and Zhou, D., 1992, "Experimental Investigation of Reynolds Shear Stresses and Heat fluxes in a Transitional Boundary Layer, " ASME HTD Vol. 226, Fundamental and Applied Heat Transfer Research for Gas Turbine Engines, pp. 61-70.
27. Wang, T., Keller, F.J., and Thou, D., 1996, "Flow and Thermal Structures in a Transitional Boundary Layer, " Experimental Thermal and Fluid Science, Vol. 12, pp.352-363.
28. Wang, T. and Thou, D., 1997, "Conditionally Sampled Row and Thermal Structures of a Transitional Boundary Layer at Elevated Free-Stream Turbulence, " to be presented at the ASME Fluid Engineering Summer Meeting, Vancouver, Canada.