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A boundary element analysis of quasi-potential inviscid incompressible flow in multiply connected airfoil wing
https://orcid.org/http://orcid.org/0000-0002-2417-3913
The quasi-potential flow in a doubly linked airfoil wing with a sharp trailing edge can be solved using a high-order boundary-element method (BEM). A bicubic Hermite spline interpolation is used to express the unknown, with node derivatives given by finite difference method. The revolutionary traits apply to bleeding-edge settings; specifically, challenges relating to the three-dimensional problem of multiply connected domains are investigated. Numerical validation examples were utilized to assess the implemented BEM approach.
A boundary element analysis of quasi-potential inviscid incompressible flow in multiply connected airfoil wing
https://orcid.org/http://orcid.org/0000-0002-2417-3913
The quasi-potential flow in a doubly linked airfoil wing with a sharp trailing edge can be solved using a high-order boundary-element method (BEM). A bicubic Hermite spline interpolation is used to express the unknown, with node derivatives given by finite difference method. The revolutionary traits apply to bleeding-edge settings; specifically, challenges relating to the three-dimensional problem of multiply connected domains are investigated. Numerical validation examples were utilized to assess the implemented BEM approach.
A boundary element analysis of quasi-potential inviscid incompressible flow in multiply connected airfoil wing
https://orcid.org/http://orcid.org/0000-0002-2417-3913
The quasi-potential flow in a doubly linked airfoil wing with a sharp trailing edge can be solved using a high-order boundary-element method (BEM). A bicubic Hermite spline interpolation is used to express the unknown, with node derivatives given by finite difference method. The revolutionary traits apply to bleeding-edge settings; specifically, challenges relating to the three-dimensional problem of multiply connected domains are investigated. Numerical validation examples were utilized to assess the implemented BEM approach.
A boundary element analysis of quasi-potential inviscid incompressible flow in multiply connected airfoil wing
J. Umm Al-Qura Univ. Eng.Archit.
Fahmy, Mohamed Abdelsabour (author) / Alzubaidi, Mohammed Hassan M. (author)
2024-12-01
5 pages
Article (Journal)
Electronic Resource
English
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