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- W2304244498 abstract "In this paper we consider the solution of the compressible Navier-Stokes equations for a class oflaminar airfoil flows. The principal objective of this paper is to demonstrate that members of thisclass of laminar flows have steady-state solutions. These laminar airfoil flow cases are often used toevaluate accuracy, stability and convergence of numerical solution algorithms for the Navier-Stokesequations. In recent years, such flows have also been used as test cases for high-order numericalschemes. While generally consistent steady-state solutions have been obtained for these flows usinghigher order schemes, a number of results have been published with various solutions, includingunsteady ones. We demonstrate with two different numerical methods and a range of meshes witha maximum density that exceeds 8 × 10^6 grid points that steady-state solutions are obtained. Furthermore,numerical evidence is presented that even when solving the equations with an unsteadyalgorithm, one obtains steady-state solutions." @default.
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- W2304244498 date "2016-01-01" @default.
- W2304244498 modified "2023-09-24" @default.
- W2304244498 title "Comparison of NACA 0012 Laminar Flow Solutions: Structured and Unstructured Grid Methods" @default.
- W2304244498 hasPublicationYear "2016" @default.
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