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An Improved Finite Element Formulation for Potential Flow Problems Using a Kutta Condition
Journal Article
01-15-01-0007
ISSN: 1946-3855, e-ISSN: 1946-3901
Sector:
Topic:
Citation:
Reddy, S. and Deb, A., "An Improved Finite Element Formulation for Potential Flow Problems Using a Kutta Condition," SAE Int. J. Aerosp. 15(1):99-117, 2022, https://doi.org/10.4271/01-15-01-0007.
Language:
English
Abstract:
The purpose of the present article is to develop a Finite Element Method (FEM)
for steady potential flows over a range of bluff bodies like cylinders to
streamlined profiles such as airfoils. In contrast to conventional panel
methods, Laplace’s equation describing the potential flow is solved here for the
velocity-potential function using the Galerkin method. A brief discussion on
edge singularities in potential flows has also been presented using a
half-cylinder case study. A novel method for implementing Kutta condition over
airfoils to have lifting flow is explained. Compared with other techniques such
as Finite Difference Method (FDM) and Finite Volume Method (FVM), the present
methodology has proven to be computationally faster for airfoils with both a
finite angle trailing edge and cusped trailing edge. The results obtained have
demonstrated excellent accuracy compared to analytical and panel methods. The
present method has also overcome edge singularity for airfoils, which ANSYS
Fluent predicted inappropriately using the inviscid model.