Solutions for incompressible separated boundary layers including viscous-inviscid interaction

Numerical solutions are presented for the laminar and turbulent boundary-layer equations for incompressible flows with separation and reattachment. The separation singularity is avoided by using an inverse technique in which the displacement thickness is prescribed and the pressure is deduced from the resulting solution. The turbulent results appear qualitatively-correct despite the use of a two-layer eddy-viscosity model which is generally assumed appropriate only for mild-pressure-gradient flows. A new viscous-inviscid interaction technique is presented in which the inviscid flow is solved inversely by prescribing the pressure from the boundary-layer solution and deducing the new displacement thickness from the solution of a Cauchy integral. Calculations are presented using this interaction procedure for a laminar flow in which separation and reattachment occur on a solid surface.

[1]  J. Steger,et al.  On laminar boundary-layer separation , 1974 .

[2]  D. Catherall,et al.  The integration of the two-dimensional laminar boundary-layer equations past the point of vanishing skin friction , 1966, Journal of Fluid Mechanics.

[3]  J. Carter Solutions for laminar boundary layers with separation and reattachment , 1974 .

[4]  K. Stewartson,et al.  On the flow near the trailing edge of a flat plate II , 1969 .

[5]  W. Roger Briley,et al.  Numerical prediction of incompressible separation bubbles , 1975, Journal of Fluid Mechanics.

[6]  Tuncer Cebeci,et al.  Accurate Numerical Methods for Boundary-Layer Flows. II: Two Dimensional Turbulent Flows , 1971 .

[7]  I. Flügge-Lotz,et al.  The interaction of a shock wave with a laminar boundary layer , 1968 .

[8]  T. Tai Transonic Laminar Viscous-inviscid Interaction over Airfoils , 1975 .

[9]  J. Carter,et al.  Forward marching procedure for separated boundary-layer flows , 1975 .

[10]  J. E. Carter Numerical solutions of the Navier-Stokes equations for the supersonic laminar flow over a two-dimensional compression corner , 1972 .

[11]  J. E. Harris Numerical solution of the equations for compressible laminar, transitional, and turbulent boundary layers and comparisons with experimental data , 1971 .

[12]  R. Melnik,et al.  Asymptotic theory of two-dimensional trailing-edge flows , 1975 .

[14]  F. G. Blottner,et al.  Variable grid scheme applied to turbulent boundary layers , 1974 .

[15]  K. Stewartson On the flow near the trailing edge of a flat plate , 1968, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[16]  Prediction of Turbulent Separated Boundary Layers , 1974 .

[17]  H. L. Morgan,et al.  Mathematical model for two-dimensional multi-component airfoils in viscous flow. , 1972 .

[18]  V. Vatsa,et al.  New Method for Supersonic Boundary-Layer Separations , 1974 .

[19]  J. Cole,et al.  Calculation of plane steady transonic flows , 1970 .

[20]  D. Dwoyer SUPERSONIC AND HYPERSONIC TWO-DIMENSIONAL LAMINAR FLOW OVER A COMPRESSION CORNER , 1973 .

[21]  O. Burggraf,et al.  The numerical solution of the asymptotic equations of trailing edge flow , 1974, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.