Abstract
A predictor-corrector multiple iteration method is formulated to treat three-dimensional viscous flow problems. Specific application is made to the viscous interaction near a hypersonic leading edge. The effects of iteration on accuracy, stability and consistency of the finite-difference solutions is evaluated for both leading-edge calculations and a model Burgers' equation. For a right-angle corner geometry comparisons are made with explicit finite-difference solutions and some recent experimental data.
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