4.7 Article

Isogeometric fluid-structure interaction analysis with emphasis on non-matching discretizations, and with application to wind turbines

出版社

ELSEVIER SCIENCE SA
DOI: 10.1016/j.cma.2012.03.028

关键词

Isogeometric analysis; NURBS; T-splines; Fluid-structure interaction; Non-matching interface discretizations; NREL 5 MW offshore wind turbine rotor

资金

  1. Los Alamos-UC San Diego Educational Collaboration Fellowship
  2. NSF CAREER Award [1055091]
  3. Air Force Office of Scientific Research Award [FA9550-12-1-0005]
  4. CAM Graduate Fellowship at the Institute for Computational Engineering and Sciences (ICES), the University of Texas at Austin
  5. Office of Advanced Cyberinfrastructure (OAC)
  6. Direct For Computer & Info Scie & Enginr [1055091] Funding Source: National Science Foundation

向作者/读者索取更多资源

In this paper we develop a framework for fluid-structure interaction (FSI) modeling and simulation with emphasis on isogeometric analysis (IGA) and non-matching fluid-structure interface discretizations. We take the augmented Lagrangian approach to FSI as a point of departure. Here the Lagrange multiplier field is defined on the fluid-structure interface and is responsible for coupling of the two subsystems. Thus the FSI formulation does not rely on the continuity of the underlying function spaces across the fluid-structure interface in order to produce the correct coupling conditions between the fluid and structural subdomains. However, in deriving the final FSI formulation the interface Lagrange multiplier is formally eliminated and the formulation is written purely in terms of primal variables. Avoiding the use of Lagrange multipliers adds efficiency to the proposed formulation. As an added benefit, the ability to employ non-matching grids for multi-physics simulations leads to significantly relaxed requirements that are placed on the geometry modeling and meshing tools for IGA. We show an application of the proposed FSI formulation to the simulation of the NREL 5 MW offshore wind turbine rotor, where the aerodynamics domain is modeled using volumetric quadratic NURBS, while the rotor structure is modeled using a cubic T-spline-based discretization of a rotation-free Kirchhoff-Love shell. We conclude the article by showing FSI coupling of a T-spline shell with a low-order finite element method (FEM) discretization of the aerodynamics equations. This combined use of IGA and FEM is felt to be a good balance between speed, robustness, and accuracy of FSI simulations for this class of problems. (C) 2012 Elsevier B.V. All rights reserved.

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