Affiliation:
1. Rensselaer Polytechnic Institute, Department of Mechanical, Aerospace and Nuclear Engineering, Troy, NY 12180
Abstract
In his now classical paper on pressure gradient turbulent boundary layers, Clauser concluded that equilibrium flows were very special flows difficult to achieve experimentally and that few flows were actually in equilibrium [1]. However, using similarity analysis of the Navier–Stokes equations, Castillo and George [2] defined an equilibrium flow as one where the pressure parameter, Λ=[δ/ρU∞2dδ/dx]dP∞/dx, was a constant. They further showed that most flows were in equilibrium and the exceptions were nonequilibrium flows where Λ≠constant. Using the equations of motion and similarity analysis, it will be shown that even nonequilibrium flows, as those over airfoils or with sudden changes on the external pressure gradient, are in equilibrium state, but only locally. Moreover, in the case of airfoils where the external pressure gradient changes from favorable to zero then to adverse, three distinctive regions are identified. Each region is given by a constant value of Λθ, and each region remains in equilibrium with Λθ=constant, respectively.
Reference35 articles.
1. Clauser, F. H. , 1956, “The Turbulent Boundary Layer,” Adv. Appl. Mech., 4, pp. 1–54.
2. Castillo, L., and George, W. K., 2001, “Similarity Analysis for Turbulent Boundary Layer With Pressure Gradient: Outer Flow,” AIAA J., 39, pp. 41–47.
3. Bradshaw, P. , 1967, “The Turbulent Structure of Equilibrium Boundary Layers,” J. Fluid Mech., 29, pp. 624–645.
4. Townsend, A. A., 1956, The Structure of Turbulent Shear Flow, Cambridge University Press, London.
5. Rotta, J. C., 1962, “Turbulent Boundary Layers in Incompressible Flow,” Progr. Aeronautical Sci., Vol. 2., Pergamon, New York.
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