Fluid-Structure Interaction of a wing (Αλληλεπίδραση πτέρυγας – αέρος)
Journal
Computer Methods in Applied Mechanics and Engineering
Date Issued
2007
Author(s)
Abstract
In this paper a new mesh update technique is proposed combined with a PCG-based algorithm, for the solution of 3D mesh moving boundary problems. The PCG-based algorithm is also applied to three other mesh updating techniques, namely the torsional, the semi-torsional and the ball-vertex spring analogy schemes. The robustness of these four spring analogy methods is evaluated and their computational efficiencies are compared in 3D benchmark problems, including the AGARD wing 445.6 and a 3D three-element airfoil. It is demonstrated that the ortho-semi-torsional spring analogy concept, in conjunction with a PCG type method for the solution of fictitious elasticity problems, provides robustness for substantially distorted meshes and computational efficiency for large scale problems.
Affiliation
Funding
ΕΑΒ, Greek Aviation Industry
Scopus Subject Areas
Computational Mechanics
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Mechanics of Materials
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Mechanical Engineering
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Physics and Astronomy (all)
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Computer Science Applications

