NASA NTRS ยท 19810016798
A modified dodge algorithm for the parabolized Navier-Stokes equations and compressible duct flows
Abstract
A revised version of a split-velocity method for numerical calculation of compressible duct flow was developed. The revision incorporates balancing of mass flow rates on each marching step in order to maintain front-to-back continuity during the calculation. The (checkerboard) zebra algorithm is applied to solution of the three-dimensional continuity equation in conservative form. A second-order A-stable linear multistep method is employed in effecting a marching solution of the parabolized momentum equations. A checkerboard successive overrelaxation iteration is used to solve the resulting implicit nonlinear systems of finite-difference equations which govern stepwise transition.
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Cooke, C. H.. 1981-06-01. A modified dodge algorithm for the parabolized Navier-Stokes equations and compressible duct flows. https://ntrs.nasa.gov/citations/19810016798
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