Abstract
A proven inviscid algorithm (Program EAGLE - Flow Solver) has been modified to use the flux-difference split scheme of Roe to solve the time-lagged, thin-layer approximation to the Navier-Stokes equations. Calculations are presented evaluating the ability of the time-lagged, thinlayer Navier-Stokes algorithm to obtain transonic solutions for lifting bodies at incidence angles sufficient for the flow to be dominated by large-scale free vortices in the leeside flowfield.
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Schedule a callMore From: AIAA journal. American Institute of Aeronautics and Astronautics
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