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《Aircraft Design》 2006-04
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Analyses & Validation of an Aircraft Cockpit Canopy Finite Element Model

WANG Jia-ying,DI Xiang-fa(Shenyang Aircraft Design & Research Institute,Shenyang110035,China)  
"PATRAN" is used to create a canopy FEM for an aircraft using MPC to simulate the flexible attachment between plexiglass and frame.Through "NASTRAN" calculation,the stress distribution on the canopy plexiglass is obtained and the critical part of the canopy is determined.The test validation is conducted.
【CateGory Index】: V223
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