Kalkan, A., & Mecitoğlu, Z. (2017). A METHOD BASED ON CLASSICAL LAMINATION THEORY TO CALCULATE STIFFNESS PROPERTIES OF CLOSED COMPOSITE SECTIONS. Journal of Aeronautics and Space Technologies, 10(1), 31–44. Retrieved from https://jast.hho.msu.edu.tr/index.php/JAST/article/view/25