mechanical testing;
elastic and plastic behavior;
buckling analysis;
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摘要:
The effects of the length, sector angle, and different boundary conditions on the buckling load and post buckling behavior of cylindrical panels have been investigated using experimental and numerical methods. The experimental tests have been performed using a servo-hydraulic machine, Instron 8808, and for numerical analysis, Abaqus finite element package has been used. The numerical results are in good agreement with the experimental tests.
机构:
State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and AstronauticsState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics
Yan HUANG
Yahui ZHANG
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机构:
AVIC Aviation Power Control System Research InstituteState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics
Yahui ZHANG
Bin KONG
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机构:
Chengdu Aircraft Design and Research Institute,Aviation Industry Corporation of ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics
Bin KONG
Jiefei GU
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机构:
School of Mechanical Engineering,Jiangnan UniversityState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics
Jiefei GU
Zhe WANG
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机构:
School of Aeronautic Science and Engineering,Beihang University
China National Key Laboratory of Strength and Structural Integrity,Aircraft Strength Research Institute ofState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics
Zhe WANG
Puhui CHEN
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机构:
State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and AstronauticsState Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics and Astronautics