Bypass transition in boundary layers including curvature and favorable pressure gradient effects

Journal of Turbomachinery

Volumn 117, Issue 1, 1995, Pages 166-174

  Volino, R J ^a   Simon, T W ^a  

^a UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; ENTHALPY; PRESSURE EFFECTS; REYNOLDS NUMBER; TRANSITION FLOW; TURBULENCE; TURBULENT FLOW; VORTEX FLOW;

BYPASS TRANSITION; FREE STREAM DISTURBANCE; INTERMITTENCY; MOMENTUM THICKNESS REYNOLDS NUMBER; PRESSURE GRADIENT EFFECTS; SKIN FRICTION COEFFICIENTS; STANTON NUMBER; STREAMWISE ACCELERATION;

BOUNDARY LAYERS;

BOUNDARY LAYERS; PRESSURE; TRANSITION;

EID: 0029140055     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2835634     Document Type: Article

References (35)

1. Abu-Ghannam, B. J., and Shaw, R., 1980, “Natural Transition of Boundary Layers-The Effects of Turbulence, Pressure Gradient, and Flow History,” J. Mechanical Engineering Science, Vol. 22, No. 5, pp. 213-228.
2. Blair, M. F., and Wcrlc, M. J., 1980, “The Influence of Free-Stream Turbulence on the Zero Pressure Gradient Fully Turbulent Boundary Layer,” United Technologies Research Center report R80-914388-12.
3. Blair, M. F., 1981a, “Final Data Report-Vol. I -Velocity and Temperature Profile Data for Zero Pressure Gradient, Fully Turbulent Boundary Layers,” United Technologies Research Center report R8I-914388-15.
4. Blair, M. F., 1981b, “Final Data Report-Vol. II-Velocity and Temperature Profile Data for Accelerating, Transitional Boundary Layers,” United Technologies Research Center report R81-914388-16.
5. Blair, M. F., and Werle, M. J., 1981, “Combined Influence of Free-Strcam Turbulence and Favorable Pressure Gradients on Boundary Layer Transition and Heat Transfer,” United Technologies Research Center report R81-914388-17.
6. Blair, M. F., 1982, “Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients,” ASME Journal of Engineering for Power, Vol. 104, pp. 743-750.
7. Blair, M. F., 1983, “Influence of Frec-Strcam Turbulence on Turbulent Boundary Layer Heat Transfer and Mean Profile Development, Part I, Experimental Data,” ASME Journal of Heat Transfer, Vol. 105, pp. 33-40.
8. Blair, M. F., and Anderson, O. L., 1987, “Study of the Structure of Turbulence in Accelerating Transitional Boundary Layers,” United Technologies Research Center report R87-956900-1.
9. Chen, K. K., and Thyson, N. A., 1971, “Extension of Emmons’ Spot Theory to Flows on Blunt Bodies,” A/AA Journal, Vol. 9, pp. 821-825.
10. Crawford, M. E., and Kays, W. M., (1976), “STAN5 - A Program for Numerical Computation of Two-Dimensional Internal and External Boundary Layer Flows,” NASA CR-2742.
11. Dhawan, S., and Narasimha, R., 1958, “Some Properties of Boundary Layer Flow During the Transition From Laminar to Turbulent Motion,” J. Fluid Mech., Vol. 3, pp. 418-436.
12. Emmons, H. W., 1951, “The Laminar-Turbulent Transition in a Boundary Layer-Part I,” J. Aeronautical Science, Vol. 18, pp. 490-498.
13. Gostelow, J. P., and Walker, G. J., 1991, “Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels,” ASME Journal of Turuomaciiinery, Vol. 113, pp. 617-625.
14. Kays, W. M., and Crawford, M. E., 1993, Convective Heat and Mass Transfer, McGraw-H3, New York.
15. Kim, J., Simon, T. W., and Kestoras, M., 1994, “Fluid Mechanics and Heat Transfer Measurements in Transitional Boundary Layers Conditionally Sampled on Intermittcncy,” ASME Journal of Turhomaciiin-ery, Vol. 116, pp. 405-416.
16. Kim, J., Simon, T. W., and Russ, S., 1992, “Frce-Strcam Turbulence and Concave Curvature Effects on Heated Transitional Boundary Layers,” ASME Journal of Heat Transfer, Vol. 114, pp. 338-347.
17. Kim, J., and Simon, T. W., 1991, “Free-Stream Turbulence and Concave Curvature Effects on Heated, Transitional Boundary Layers. Vol. I -Final Report,” NASA CR 187150; “Vol. II-Program Listings and Tabulated Data,” NASA CR 187151
18. Kuan, C. L., 1987, “An Experimental Investigation of Intermittent Behavior in the Transitional Boundary Layer,” M.S. Thesis, Clemson University, Clemson, SC.
19. Kuan, C. L., and Wang, T., 1990, “Investigation of the Intermittent Behavior of Transitional Boundary Layer Using a Conditional Averaging Technique,” Experimental Thermal and Fluid Science, Vol. 3, pp. 157-173.
20. Maylc, R. E., 1991, “The Role of Laminar-Turbulent Transition in Gas Turbine Engines,” ASME Journal of Turbomaciiinery, Vol. 113, pp. 509-537.
21. McDonald, H., and Fish, R. W., 1973, “Practical Calculation of Transitional Boundary Layers,” Int. J. Heat Mass Transfer, Vol. 16, pp. 1729-1744.
22. Morkovin, M. V., 1978, “Instability, Transition to Turbulence and Predictability,” AGARD-AG-236.
23. Narasimha, R., 1984, “Subtransitions in the Transition Zone,” Proc. 2nd IUTAM Symposium on Laminar-Turbulent Transition, Novosibirsk, pp. 141-151.
24. Narasimha, R., 1985, “The Laminar-Turbulent Transition Zone in the Boundary Layer,” Progress in Aerospace Science, Vol. 22, No. 1, pp. 29-80.
25. Rued, K., and Wittig, S., 1985, “Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 54-59.
26. Rued, K., and Wittig, S., 1986, “Laminar and Transitional Boundary Layer Structures in Accelerating Flow with Heat Transfer,” ASME Journal of Turbomachinery, Vol. 108, pp. 116-123.
27. Rued, K„ 1987, “Transitional Boundary Layers Under the Influence of High Free Stream Turbulence, Intensive Wall Cooling and High Pressure Gradients in Hot Gas Circulation,” NASA TM-88524.
28. Schlichting, H., 1979, Boundary Layer Theory, 7th ed., McGraw-H3, New York.
29. Sohn, K. H., O’Brien, J. E., and Reshotko, E., 1989, “Some Characteristics of Bypass Transition in a Heated Boundary Layer,” NASA TM-102126.
30. 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.
31. Van Driest, E. R., and Blumer, C. B., 1963, “Boundary Layer Transition: Freestream Turbulence and Pressure Gradient Effects,” AJAA Journal, Vol. 1, No. 6, pp. 1303-1306.
32. Volino, R. J., and Simon, T. W., 1991, “Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects,” NASA CR-187187.
33. Wang, T., 1984, “An Experimental Investigation of Curvature and Freestream Turbulence Effects on Heat Transfer and Fluid Mechanics in Transitional Boundary Layer Flows,” Ph.D. Thesis, Department of Mechanical Engineering, U. of Minnesota.
34. Wang, T., Simon, T. W., and Buddhavarapu, J., 1985, “Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layer Flows,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 1007-1015.
35. Wang, T., and Simon, T. W., 1987, “Heat Transfer and Fluid Mechanics Measurements in a Boundary Layer Undergoing Transition on a Convex-Curved Wall,” ASME Journal of Turbomachinery, Vol. 109, No. 3, pp. 443-452