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Journal of Turbomachinery-transactions of The Asme | 1995

Bypass Transition in Boundary Layers Including Curvature and Favorable Pressure Gradient Effects

Ralph J. Volino; Terrence W. Simon

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 Gortler 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 intended 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


Journal of Turbomachinery-transactions of The Asme | 1994

An Application of Octant Analysis to Turbulent and Transitional Flow Data

Ralph J. Volino; Terrence W. Simon

A technique called “octant analysis” was used to examine the eddy structure of turbulent and transitional heated boundary layers on flat and curved surfaces. The intent was to identify important physical processes that play a role in boundary layer transition on flat and concave surfaces. Octant processsing involves the partitioning of flow signals into octants based on the instantaneous signs of the fluctuating temperature, t′, streamwise velocity, u′, and cross-stream velocity, v′. Each octant is associated with a particular eddy motion. For example, u′ 0, t′>0 is associated with an ejection or “burst” of warm fluid away from a heated wall. Within each octant, the contribution to various quantities of interest (such as the turbulent shear stress, −u′v′ , or the turbulent heat flux, v′t′ ) can be computed. By comparing and contrasting the relative contributions from each octant, the importance of particular types of motion can be determined. If the data within each octant are further segregated based on the magnitudes of the fluctuating components so that minor events are eliminated, the relative importance of particular types of motion to the events that are important can also be discussed. In fully developed, turbulent boundary layers along flat plates, trends previously reported in the literature were confirmed. A fundamental difference was observed in the octant distribution between the transitional and fully turbulent boundary layers, however, showing incomplete mixing and a lesser importance of small scales in the transitional boundary layer. Such observations were true on both flat and concave walls. The differences are attributed to incomplete development of the turbulent kinetic energy cascade in transitional flows. The findings have potential application to modeling, suggesting the utility of incorporating multiple length scales in transition models.


Journal of Heat Transfer-transactions of The Asme | 1997

Boundary Layer Transition Under High Free-Stream Turbulence and Strong Acceleration Conditions: Part 2—Turbulent Transport Results

Ralph J. Volino; Terrence W. Simon


Journal of Heat Transfer-transactions of The Asme | 1997

Boundary Layer Transition Under High Free-Stream Turbulence and Strong Acceleration Conditions: Part 1—Mean Flow Results

Ralph J. Volino; Terrence W. Simon


American Society of Mechanical Engineers, Heat Transfer Division, (Publication) HTD | 1995

Evaluation of local wall temperature, heat flux, and convective heat transfer coefficient from the near-wall temperature profile

Songgang Qiu; Terrence W. Simon; Ralph J. Volino


Archive | 1996

Separating and Separated Boundary Layers.

Terrence W. Simon; Ralph J. Volino


Transactions of the ASME. Serie C: Journal of heat transfer | 1997

Boundary layer transition under high free-stream turbulence and strong acceleration conditions

Ralph J. Volino; Terrence W. Simon


Transactions of the ASME. Serie C: Journal of heat transfer | 1997

Velocity and temperature profiles in turbulent boundary layer flows experiencing streamwise

Terrence W. Simon; Ralph J. Volino


ASME. Winter annual meeting | 1995

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

Ralph J. Volino; Terrence W. Simon


Proceedings of the 1994 International Mechanical Engineering Congress and Exposition | 1994

Velocity and temperature profiles in turbulent boundary layer flows experiencing streamwise pressure gradients

Ralph J. Volino; Terrence W. Simon

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Songgang Qiu

University of Minnesota

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