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

Han Qi Zhu; Nai Ming Wu

doi:10.4028/www.scientific.net/AMM.668-669.197

Paper Titles

Finite Analytic Method for 2D Fluid Flows in Porous Media with Full Tensor Permeability
p.181

Finite Element Analysis of Pipe Joints under Torsion Load
p.185

Force Analysis on Piston Assembly of Mine Rotor Wet Spraying Machine
p.189

Free Vibration of High-Rise Chemical Tower Controlled by Super-Elastic Shape Memory Alloy Cables
p.193

Joint Application of UG/ADAMS/ANSYS in the Analysis of Landing Gear
p.197

Mechanical Characters of Six Engineering Timoshenko Beams
p.201

Mixed Lubrication and Friction Power Loss of Piston Ring Pack
p.205

Modal Analysis and Unbalanced Response Analysis of Rotor System
p.209

Modification of Finite Element Modeling and Analysis on Various Factors of Rupture during Square Plansifter Running
p.213

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 668-669Joint Application of UG/ADAMS/ANSYS in the...

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

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.