A multigrid algorithm for steady transonic potential flows around aerofoils using Newton iteration

DOI10.1016/0021-9991(82)90055-9zbMath0507.76061OpenAlexW2138751960MaRDI QIDQ1837583

J. W. Boerstoel

Publication date: 1982

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-9991(82)90055-9

zbMATH Keywords

multigrid algorithmshock-positions

Mathematics Subject Classification ID

Mesh generation, refinement, and adaptive methods for boundary value problems involving PDEs (65N50) Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)

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Cites Work

• On the fast solutions of nonlinear elliptic equations
• Implicit Algorithm for the Conservative Transonic Full-Potential Equation Using an Arbitrary Mesh
• Iterative solution of transonic flows over airfoils and wings, including flows at mach 1
• Multi-Level Adaptive Solutions to Boundary-Value Problems
• Numerical Calculation of Transonic Potential Flow about Wing-Body Combinations
• Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential Equation
• Analysis of Embedded Shock Waves Calculated by Relaxation Methods
• Calculation of plane steady transonic flows