NASA NTRS · 19760031018
Forward marching procedure for separated boundary-layer flows
Abstract
A forward-marching procedure for separated boundary-layer flows which permits the rapid and accurate solution of flows of limited extent is presented. The streamwise convection of vorticity in the reversed flow region is neglected, and this approximation is incorporated into a previously developed (Carter, 1974) inverse boundary-layer procedure. The equations are solved by the Crank-Nicolson finite-difference scheme in which column iteration is carried out at each streamwise station. Instabilities encountered in the column iterations are removed by introducing timelike terms in the finite-difference equations. This provides both unconditional diagonal dominance and a column iterative scheme, found to be stable using the von Neumann stability analysis.
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Carter, J. E., Wornom, S. F.. 1975-08-01. Forward marching procedure for separated boundary-layer flows. https://ntrs.nasa.gov/citations/19760031018
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