Fast Euler solver for transonic airfoils. I - Theory. II - Applications

DOI10.2514/3.9909zbMath0665.76061OpenAlexW1992251884MaRDI QIDQ3817985

Gino Moretti, Andrea Dadone

Publication date: 1988

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.9909

zbMATH Keywords

airfoilC gridgeneralized Riemann variablesShocksimplicit Euler solver\(\lambda \) -formulation

Mathematics Subject Classification ID

Transonic flows (76H05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (5)

Three-dimensional flow computations with shock fitting ⋮ On high-order shock-fitting and front-tracking schemes for numerical simulation of shock-disturbance interactions ⋮ Numerical simulation of shock/boundary-layer interaction using an unstructured shock-fitting technique ⋮ Computations of viscous flows using a multigrid finite volume lambda formulation ⋮ Thirty-six years of shock fitting.

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