相关期刊:《Transactions of Nanjing University of Aeronautics and Astronautics》《Applied Mathematics and Mechanics(English Edition)》《Defence Technology(防务技术)》《应用力学学报》更多>>
Project supported by the National Natural Science Foundation of China(Nos.11832002 and 12072201)。
The chaotic dynamic snap-through and complex nonlinear vibrations are investigated in a rectangular asymmetric cross-ply bistable composite laminated cantilever shell,in cases of 1:2 inter-well internal resonance and ...
the Research Foundation for Advanced Talents of Jiangsu University(15JDG038);the Foundation of National Laboratory(601010417);the Natural Science Foundation of the Jiangsu Higher Education Institutions of China(19KJB130003).
Cross-ply unidirectional laminates made of ultra-high molecular weight polyethylene fibers are widely used as components of bullet-proof vests.To simulate the delamination process of the material under penetration,we ...
co-supported by the National Natural Science Foundation of China (Nos. 11372021 and 11672019);Research Fund for the Doctoral Program of Higher Education of China (No. 20131102110039)
Based on the first-order shear deformation theory, this paper explores the analytical methods for eigenbuckling of symmetric cross-ply rectangular composite laminates with a pair of parallel edges simply supported and...
This paper presents the stress resultants of hyperbolic paraboloidal shells using higher order shear deformation theory recently developed by Zannon [1]-[3]. The equilibrium equations of motion use Hamilton’s minimum...
supported by the National Natural Science Foundation of China(Nos.11172113,11032005,and 11072037)
The conventional approach to analysis the buckling of rectangular laminates containing an embedded delamination subjected to the in-plane loading is to simplify the laminate as a beam-plate from which the predicted bu...
Supported by the Graduate Innovation Foundation of Jiangsu Province(CX08B-133Z);the Doctoral Innovation Foundation of Nanjing University of Aeronautics and Astronautics(BCXJ08-05)~~
The matrix crack evolution of cross-ply ceramic matrix composites under uniaxial tensile loading is investigated using the energy balance method.Under tensile loading,the cross-ply ceramic matrix composites have five ...
In this paper, general equations relating to the stability of laminated plates ofsymmetric cross-ply with initial imperfection factors are derived by using thevariational principle. Taking the deflection as the pertu...
A study is conducted on the creep behaviour of T300/5222 compositelaminate by expenmental and theoretical researches. Experimental results of creep,stress relaxation and historydependent stress-strain curves at differ...
A creep buckling analysis of cross-ply symmetric laminated cylindrical panels was given here. By means of theoretical analysis, a method to determine the critical load of creep buckling of the panels with simply suppo...