Hai Qing
Nanjing University of Aeronautics and Astronautics
Composite numberUltimate tensile strengthPhysicsMathematical analysisFinite element methodComposite materialBoundary value problemMaterials scienceConstitutive equationIntegral modelFiberMechanicsStructural engineeringBendingMicrostructureStress (mechanics)Laplace transform
56Publications
14H-index
659Citations
Publications 61
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#1Pei-Liang Bian (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 4
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
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#1Pei-Liang Bian (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 4
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
Last. Siegfried Schmauder (University of Stuttgart)H-Index: 37
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#1Pei Zhang (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 15
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
The thermoelastic analysis is extremely important due to the highly integrated characteristics in micro- and nano-electro-mechanical systems. In this paper, thermal flux driven (TFD) and temperatur...
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#1Pei Zhang (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 15
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
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#1Pei Zhang (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 15
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
It is well-acknowledged by the scientific community that Eringen’s nonlocal integral theory is not applicable to nanostructures of engineering interest due to conflict between equilibrium and const...
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Abstract In this work, nonlocal strain gradient integral model is applied to study the elastic buckling and free vibration response of functionally graded (FG) Timoshenko beam which is made of two constituents varying along thickness direction. The differential governing equations and corresponding boundary conditions are derived via the Hamilton's principle, and the relations between nonlocal stresses and strains are expressed as integral equations. The Laplace transform technique is applied to...
1 CitationsSource
#1Pei-Liang Bian (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 4
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
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#1Pei Zhang (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 15
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
Due to the conflict between equilibrium and constitutive requirements, Eringen’s strain-driven nonlocal integral model is not applicable to nanostructures of engineering interest. As an alternative, the stress-driven model has been recently developed. In this paper, for higher-order shear deformation beams, the ill-posed issue (i.e., excessive mandatory boundary conditions (BCs) cannot be met simultaneously) exists not only in strain-driven nonlocal models but also in stress-driven ones. The wel...
2 CitationsSource
#1Yan-Ming Ren (NUAA: Nanjing University of Aeronautics and Astronautics)
#2Hai Qing (NUAA: Nanjing University of Aeronautics and Astronautics)H-Index: 14
Static bending and elastic buckling of Euler–Bernoulli beam made of functionally graded (FG) materials along thickness direction is studied theoretically using stress-driven integral model with bi-...
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