Boundary element method for the analysis of the unsteady flow aroundextreme propeller geometries

DOI10.2514/3.10973zbMath0766.76053OpenAlexW1966675097MaRDI QIDQ4036310

Ching-Yeh Hsin, Spyros A. Kinnas

Publication date: 16 May 1993

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

Full work available at URL: https://doi.org/10.2514/3.10973

zbMATH Keywords

dipole distributionsexplicit Kutta conditionquadrilateral panelsspatially nonuniform inflowtime-marching potential-based low-order boundary element method

Mathematics Subject Classification ID

General theory of rotating fluids (76U05) Boundary element methods applied to problems in fluid mechanics (76M15) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

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Boundary-element method for the prediction of performance of flapping foils with leading-edge separation ⋮ A boundary element-vortex particle hybrid method with inviscid shedding scheme ⋮ Fluid flows around turbomachinery using an explicit pseudo‐temporal Euler FEM ⋮ Hybrid numerical technique for evaluating wing aerodynamic loading with propeller interference ⋮ Modeling the capacity of a novel flow-energy harvester ⋮ Modeling of cavitating or ventilated flows using BEM ⋮ The local error of a low-order boundary element method at the trailing edge of a hydrofoil and its effect on the global solution

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