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Xiaojie Yuan
Researcher at Dalian University of Technology
Publications - 8
Citations - 256
Xiaojie Yuan is an academic researcher from Dalian University of Technology. The author has contributed to research in topics: Isogeometric analysis & Finite element method. The author has an hindex of 5, co-authored 7 publications receiving 169 citations.
Papers
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Journal ArticleDOI
An integrated framework of exact modeling, isogeometric analysis and optimization for variable-stiffness composite panels
TL;DR: An integrated framework of exact modeling, isogeometric analysis and optimization for variable-stiffness panels is developed for the global optimum, and the proposed method is able to provide a more efficient optimum design with significant less computational cost compared to other traditional methods.
Journal ArticleDOI
Isogeometric buckling analysis of composite variable-stiffness panels
TL;DR: In this paper, the buckling behavior of composite variable-stiffness panels is investigated based on IGA, whose main feature is that the continuity of fiber angle on the whole panel is guaranteed.
Journal ArticleDOI
Buckling optimization of variable-stiffness composite panels based on flow field function
TL;DR: In this paper, the flow field function containing a uniform field and several vortex fields is used to represent the fiber path, and a bi-level optimization framework of variable-stiffness panels considering manufacturing constraints is then proposed.
Journal ArticleDOI
Isogeometric analysis and design of variable-stiffness aircraft panels with multiple cutouts by level set method
TL;DR: The method for suppressing artificial buckling modes is proposed to improve the prediction accuracy, the analytical sensitivity is derived to facilitate fiber path optimization, and a new bi-level optimization framework considering manufacturing constraints is established.
Patent
Efficient optimization method for variable stiffness composite material plate shell structure
TL;DR: In this article, a variable stiffness composite material plate shell structure based on an isogeometric method was proposed to reduce the development period of composite material structures in aerospace structures, and the buckling response of the composite material was analyzed.