A direct boundary integral method for the three-dimensional lifting flow

DOI10.1016/0045-7825(95)00850-4zbMath0866.76050OpenAlexW2039068566MaRDI QIDQ2564594

Lazăr Dragoş, Adrian Dinu

Publication date: 23 February 1997

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(95)00850-4

zbMATH Keywords

Kutta conditionvelocity vectordiscrete distribution of inner vorticeshigh spanwise wingregularized integral formulation

Mathematics Subject Classification ID

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)

Related Items (1)

A boundary node method for airfoils based on the Dirichlet condition

Cites Work

• On the treatment of corners in the boundary element method
• Application of the boundary integral equation methods to subsonic flow past bodies and wings
• The problem of three-dimensional lifting potential flow and its solution by means of surface singularity distribution
• Low-Speed Aerodynamics
• A General Algorithm for Multidimensional Cauchy Principal Value Integrals in the Boundary Element Method
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: A direct boundary integral method for the three-dimensional lifting flow