Joint Application of UG/ADAMS/ANSYS in the Analysis of Landing Gear
Han Zhu, Nai Ming Wu
Abstract
Han Zhu, Nai Ming Wu
Abstract
The landing gear occupies an important position in the design, manufacture and use of the aircraft. But it spends a lot of time and resources in a real experiment. The rapid development of computer simulation technology makes it possible to have a virtual analysis of the landing gear. Based on typical CAD software UG, finite element simulation software ANSYS and virtual prototyping software ADAMS, a mixed rigid-flexible nose landing gear model is constructed in this paper. The joint application will play their advantages respectively.
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The landing gear occupies an important position in the design, manufacture and use of the aircraft. But it spends a lot of time and resources in a real experiment. The rapid development of computer simulation technology makes it possible to have a virtual analysis of the landing gear. Based on typical CAD software UG, finite element simulation software ANSYS and virtual prototyping software ADAMS, a mixed rigid-flexible nose landing gear model is constructed in this paper. The joint application will play their advantages respectively.
Key concepts: Landing gear, Joint (building), Software, Engineering, Virtual prototyping, CAD, Finite element method, Position (finance)