Recent experimental studies of two-dimensional boundary layers undergoing bypass transition have been reviewed to attempt to characterize the effects of free-stream turbulence level, acceleration, and wall curvature on bypass transition. Results from several studies were cast in terms of “local” boundary layer coordinates (momentum and enthalpy thickness Reynolds numbers) and compared. In unaccelerated flow on flat walls, skin friction coefficients were shown to match those from a laminar integral solution before transition and quickly adjusted to match those from a fully turbulent correlation after transition. Stanton number data also matched a correlation in the laminar region, but do not match correlation values so well in the turbulent region. The data showed that the relationship between skin friction coefficient and momentum thickness Reynolds number is unaffected by streamwise acceleration. Stanton numbers were strongly affected by acceleration, however, indicating a breakdown in Reynolds analogy. Concave curvature caused the formation of Go¨rtler vortices, which strongly influenced the skin friction. Convex curvature had an opposite, and lesser effect. The location and length of the transition region generally followed the expected trends as free-stream turbulence level, curvature, and acceleration were varied; the onset location and the transition length were extended by acceleration and convex curvature and reduced by concave curvature and enhanced turbulence. When individual cases were compared, some inconsistencies were observed. These inconsistencies indicate a need to characterize the flows to be compared more completely. Better spectral and length scale measurements of the free-stream disturbance would help in this regard. Within the transition region, the intermittency data from all the cases on flat walls (no curvature) were consistent with an intermittency distribution from the literature. Turbulent spot production rates were shown to be mostly dependent on free-stream turbulence, with a noted increase in spot production rate due to concave curvature and little effect of convex curvature. The acceleration effect on spot production rate was small for the cases studied.
Skip Nav Destination
Article navigation
January 1995
Research Papers
Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects
R. J. Volino,
R. J. Volino
Department of Mechanical Engineering, Heat Transfer Laboratory, University of Minnesota, Minneapolis, MN 55455
Search for other works by this author on:
T. W. Simon
T. W. Simon
Department of Mechanical Engineering, Heat Transfer Laboratory, University of Minnesota, Minneapolis, MN 55455
Search for other works by this author on:
R. J. Volino
Department of Mechanical Engineering, Heat Transfer Laboratory, University of Minnesota, Minneapolis, MN 55455
T. W. Simon
Department of Mechanical Engineering, Heat Transfer Laboratory, University of Minnesota, Minneapolis, MN 55455
J. Turbomach. Jan 1995, 117(1): 166-174 (9 pages)
Published Online: January 1, 1995
Article history
Received:
March 18, 1994
Online:
January 29, 2008
Citation
Volino, R. J., and Simon, T. W. (January 1, 1995). "Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects." ASME. J. Turbomach. January 1995; 117(1): 166–174. https://doi.org/10.1115/1.2835634
Download citation file:
Get Email Alerts
Related Articles
Transition on Concave Surfaces
J. Turbomach (July,2005)
Separation Control on Low-Pressure Turbine Airfoils Using Synthetic Vortex Generator Jets
J. Turbomach (October,2003)
Mixed Boundary Layer Skin Friction and Heat Transfer With Abrupt Transition
J. Heat Transfer (November,2014)
Boundary Layer Calculation for Analysis and Design
J. Fluids Eng (June,1978)
Related Proceedings Papers
Related Chapters
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Introduction
Design and Analysis of Centrifugal Compressors
Hydraulic Resistance
Heat Transfer & Hydraulic Resistance at Supercritical Pressures in Power Engineering Applications