... classical aeroplane 传统型飞机 classical lamination theory (CLT) 古典层板理论 classical thermodynamics 古典热力学 ...
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On the basis of classical lamination theory and large deflection hypotheses of plate, the equilibrium and compatibility equations of simply supported composite laminated plates were obtained.
基于经典的层合板理论及板的大挠度基本假设，得到四边简支层合板的非线性运动方程及变形协调方程；
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