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    Numerical solution of compressible viscous flows at high Reynolds numbers (1981)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A new numerical method which was used to reduce the computation time required in fluid dynamics to solve the Navier-Stokes equations at flight Reynolds numbers is described. The method is the implicit analogue of the explicit finite different method. It uses this as its first stage, while the second stage removes the restrictive stability condition by recasting the difference equations in an implicit form. The resulting matrix equations to be solved are either upper or lower block bidiagonal equations. The new method makes it possible and practical to calculate many important three dimensional, high Reynolds number flow fields on computers.
    Keywords: AERODYNAMICS
    Type: NASA-TM-81279 , A-8524
    Format: application/pdf
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