Flow solution on a dual-block grid around an airplane

DOI10.1016/0045-7825(87)90034-XzbMath0607.76011OpenAlexW2049543342MaRDI QIDQ1085703

Lars-Erik Eriksson

Publication date: 1987

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(87)90034-x

zbMATH Keywords

transfinite interpolationalgebraic grid generation procedurecranked delta wingexplicit Runge-Kutta time steppingfighter-type airplane geometriesfinite-volume Euler solverpatched dual-block grid system

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Applications to the sciences (65Z05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)

Related Items (2)

The equilibrium flux method for the calculation of flows with non- equilibrium chemical reactions ⋮ Algebraic grid generation

Cites Work

• A conservative treatment of zonal boundaries for Euler equation calculations
• Computation of flow around wings based on the Euler equations
• Computation of inviscid incompressible flow with rotation
• Practical Three-Dimensional Mesh Generation Using Transfinite Interpolation
• Absorbing Boundary Conditions for the Numerical Simulation of Waves

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