Rough- and Smooth-Wall Boundary Layer Similarity under Adverse Pressure Gradient Conditions
ORAL
Abstract
Outer layer similarity between rough- and smooth-wall boundary layers is well established for zero pressure gradient flows. Outside the roughness sublayer, which typically extends approximately 3 sand grain roughness heights above the surface, the mean velocity profile, turbulence statistics, and turbulence correlations will match between smooth- and rough-wall cases when quantities are normalized using the boundary layer thickness and the friction velocity uτ. Recent experiments have shown, however, that if the pressure gradient in terms of the dimensionless acceleration parameter, K=(ν/U∞2)(dU∞/dx), is matched between rough- and smooth-wall cases in a non-equilibrium adverse pressure gradient, similarity does not hold. The present work considers whether similarity can be achieved if the Clauser pressure gradient parameter, β=(δ*/to)(dP/dx), history is matched. Experiments will be conducted in boundary layers on rough and smooth walls with different K distributions to achieve matching β histories. Profiles of mean velocity and turbulence statistics will be measured using a two-component LDV system at multiple streamwise locations and assessed for similarity.
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Presenters
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Ralph J Volino
US Naval Academy, United States Naval Academy
Authors
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Ralph J Volino
US Naval Academy, United States Naval Academy
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Vidya Vishwanathan
US Naval Academy
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Michael P Schultz
US Naval Academy