Grid generation by elliptic partial differential equations for a tri- element augmentor-wing airfoil

DOI10.1016/0096-3003(82)90213-2zbMath0501.76012OpenAlexW2076076211WikidataQ127156083 ScholiaQ127156083MaRDI QIDQ1172473

Reese L. Sorenson

Publication date: 1982

Published in: Applied Mathematics and Computation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0096-3003(82)90213-2

zbMATH Keywords

cruise configurationgrid-generation program GRAPEtransonic full-potential approachtri-element augmentor-wing airfoilunsteady viscous flow-solver

Mathematics Subject Classification ID

Transonic flows (76H05) Mesh generation, refinement, and adaptive methods for boundary value problems involving PDEs (65N50) Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)

Related Items

Multi-block Poisson grid generator for cascade simulations, Algebraic grid generation for complex geometries, A finite volume method for numerical grid generation

Cites Work

• Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodies
• Implicit Algorithm for the Conservative Transonic Full-Potential Equation Using an Arbitrary Mesh
• Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries