Multifidelity Aeroelastic Model for Corrugated Morphing Structures

DOI Web Site 参考文献23件

書誌事項

公開日
2023-01
資源種別
journal article
DOI
  • 10.2514/1.c036692
公開者
American Institute of Aeronautics and Astronautics (AIAA)

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説明

<jats:p> In this paper, an efficient aeroelastic model for morphing structures with corrugated panels is proposed, combining different fidelities of aerodynamic models. A finite element method with an actuation model is used to analyze the structural deformation of morphing structures. A vortex lattice method and Cartesian-grid-based computational fluid dynamics are individually coupled with the structural model to build the medium- and high-fidelity aeroelastic models. Three different morphing cases are simulated with the two fidelities of aeroelastic models to understand the influence of the model fidelity on the simulation results. Based on the comparison study, a new efficient aeroelastic model is proposed where the medium-fidelity aeroelastic model speeds up the calculations in the aeroelastic loop and the high-fidelity aeroelastic model computes accurate aerodynamic characteristics and necessary actuation loads. Computational time of the proposed method is half of the high-fidelity model while maintaining the computational accuracy. </jats:p>

収録刊行物

  • Journal of Aircraft

    Journal of Aircraft 60 (1), 120-129, 2023-01

    American Institute of Aeronautics and Astronautics (AIAA)

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