Fatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads

A. Ebadi; Ehsan Selahi

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 More