An implicit Navier-Stokes solver for two-dimensional transonic shock wave-boundary layer interaction
type: Item
instance of: scholarly article
title: An implicit Navier-Stokes solver for two-dimensional transonic shock wave-boundary layer interaction
zbMATH Open document ID: 0641.76062
author: B. George
published in: Indian Journal of Pure \& Applied Mathematics
publication date: 1988-01-01T00:00:00Z
review text: A code has been developed using an implicit numerical scheme for solving the two-dimensional unsteady Navier-Stokes equations for the transonic shock wave-boundary layer interaction problem. The method is an adaptation of the implicit MacCormack scheme for viscous compressible flows. The technique is illustrated by applying it to study the flow past an 18 \% symmetric circular arc airfoil. A coordinate transformation is made use of to facilitate direct application of the method. Numerical results obtained through the software, for surface pressure distribution and skin friction exhibit reasonable agreement with those got earlier by \textit{G. S. Deiwert} [AIAA J. 13 (1975), 1355-1359 (1976; Zbl 0318.76042)] using an explicit integral scheme.
Mathematics Subject Classification ID: 76L05
Mathematics Subject Classification ID: 76D05
Mathematics Subject Classification ID: 76M99
zbMATH DE Number: 4045345
zbMATH Keywords: implicit numerical scheme
zbMATH Keywords: two-dimensional unsteady Navier-Stokes equations
zbMATH Keywords: transonic shock wave-boundary layer interaction problem
zbMATH Keywords: implicit MacCormack scheme
zbMATH Keywords: symmetric circular arc airfoil
MaRDI profile type: Publication
description: scientific article; zbMATH DE number 4045345