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Keywords = Finite element method
Number of Articles: 2
Fatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads
Volume 11, Issue 2 , October 2017, , Pages 1-11
Abstract
The purpose of this paper is to estimate the fatigue life of an airplane wing with laminated composite skin, subjected to variable mechanical and thermal loads. To achieve this aim,at first, the three-dimensional model of airplane wing was drawn in CATIA software. Then, by transferring the model to the ... Read MoreLocal Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner
Volume 11, Issue 1 , June 2017