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38th Aerospace Sciences Meeting and Exhibit
In this paper, we report an extension of the Space-Time Conservation Element and Solution Element (CE/SE) Method for solving the Navier-Stokes equations. Numerical algorithms for both structured and unstructured meshes are developed. To calculate the viscous flux terms, a 'midpoint rule' is used. In the setting of space-time flux conservation, a new and unified boundary-condition treatment for solid wall is introduced. The Navier Stokes solvers retain all favorable features of the originaldoi:10.2514/6.2000-393 fatcat:sbtbpvvo25dhdoxxtrwn47la64