A direct boundary integral equations method to subsonic flow with circulation past thin airfoils in ground effect
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Publication:1913233
DOI10.1016/0045-7825(94)00681-CzbMath0852.76026MaRDI QIDQ1913233
Publication date: 5 August 1996
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
collocation methodGreen functionsnonlinear boundary conditionvelocitycirculationNACA-4412 profileequal-pressure Kutta condition
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Cites Work
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- New application of hypersingular equations in the boundary element method
- The application of the boundary integral equations method to subsonic flow with circulation past thin airfoils in a wind tunnel
- The problem of three-dimensional lifting potential flow and its solution by means of surface singularity distribution
- Numerical solution of the equation for a thin airfoil in ground effect
- Thickness-Induced Lift on a Thin Airfoil in Ground Effect
- A General Algorithm for Multidimensional Cauchy Principal Value Integrals in the Boundary Element Method
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