2014•Applied Mechanics and MaterialsOpen access

Joint Application of UG/ADAMS/ANSYS in the Analysis of Landing Gear

Han Zhu, Nai Ming Wu

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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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What this paper is about

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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Available 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.

Key concepts: Landing gear, Joint (building), Software, Engineering, Virtual prototyping, CAD, Finite element method, Position (finance)

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