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Advanced FEs for the micropolar and geometrical nonlinear analyses of composite structures, file e384c433-38e6-d4b2-e053-9f05fe0a1d67
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206
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Technical report: Finite element structural analyses of the main landing gear of Leonardo F48 UAV, file e384c430-19a7-d4b2-e053-9f05fe0a1d67
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84
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Evaluation of Various Geometrical Nonlinearities in the Response of Beams and Shells, file e384c431-2aa4-d4b2-e053-9f05fe0a1d67
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58
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Vibration of metallic and composite shells in geometrical nonlinear equilibrium states, file e384c432-46a5-d4b2-e053-9f05fe0a1d67
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41
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Use of Lagrange polynomials to build refined theories for laminated beams, plates and shells, file e384c434-494f-d4b2-e053-9f05fe0a1d67
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41
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Accurate through-the-thickness stress distributions in thin-walled metallic structures subjected to large displacements and large rotations, file e384c432-469f-d4b2-e053-9f05fe0a1d67
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39
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The generation and validation of a CUF-based FEA model with laser-based experiments, file e384c431-1a3f-d4b2-e053-9f05fe0a1d67
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32
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Effect of large displacements on the linearized vibration of composite beams, file e384c431-ea75-d4b2-e053-9f05fe0a1d67
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32
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Advanced FEs for the micropolar and geometrical nonlinear analyses of composite structures, file e384c433-38e7-d4b2-e053-9f05fe0a1d67
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28
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Unified theory of structures based on micropolar elasticity, file e384c430-296f-d4b2-e053-9f05fe0a1d67
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27
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Technical report: Finite element structural analyses of the nose landing gear of Leonardo F48 UAV, file e384c430-1cef-d4b2-e053-9f05fe0a1d67
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25
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Evaluation of geometrically nonlinear effects due to large cross-sectional deformations of compact and shell-like structures, file e384c432-3399-d4b2-e053-9f05fe0a1d67
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25
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Mixing layer-wise and refined equivalent-single layer FEs based on Lagrange expansions, file e384c433-3d4c-d4b2-e053-9f05fe0a1d67
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25
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Effect of in-plane loadings on the free vibration of plates in nonlinear regime, file e384c430-736a-d4b2-e053-9f05fe0a1d67
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22
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Static analysis of thin-walled beams accounting for nonlinearities, file e384c434-aadd-d4b2-e053-9f05fe0a1d67
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21
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Large deflection and post-buckling of thin-walled structures by finite elements with node-dependent kinematics, file e384c432-f02d-d4b2-e053-9f05fe0a1d67
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20
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Large deflection of composite beams by finite elements with node-dependent kinematics, file e384c434-9c21-d4b2-e053-9f05fe0a1d67
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19
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Technical report: Drop-tests of the nose landing gear of Leonardo F48 UAV, file e384c430-1cee-d4b2-e053-9f05fe0a1d67
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18
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Preliminary technical report: Drop-tests of the nose landing gear of Leonardo F48 UAV, file e384c430-1f75-d4b2-e053-9f05fe0a1d67
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17
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Advanced FEs for the analysis of composite structure with global/local and node-dependent kinematics approaches, file e384c433-c1d8-d4b2-e053-9f05fe0a1d67
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17
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Preliminary technical report: Drop-tests of the main landing gear of Leonardo F48 UAV, file e384c430-1804-d4b2-e053-9f05fe0a1d67
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16
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Technical report: Drop-tests of the main landing gear of Leonardo F48 UAV, file e384c430-1f5d-d4b2-e053-9f05fe0a1d67
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16
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Popular benchmarks of nonlinear shell analysis solved by 1D and 2D CUF-based finite elements, file e384c432-89c3-d4b2-e053-9f05fe0a1d67
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16
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Preliminary technical report: Multi-body analysis of the nose landing gear of Leonardo F48 UAV, file e384c430-1805-d4b2-e053-9f05fe0a1d67
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15
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Nonlinear vibration of composite beams, plates and shells subjected to compression and shear loadings by unified finite elements and comparison with VCT experiments, file b466dc1a-7cc8-46d0-abad-b43123091654
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14
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Preliminary technical report: Finite element structural analyses of the nose landing gear of Leonardo F48 UAV, file e384c430-1a28-d4b2-e053-9f05fe0a1d67
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14
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Technical report: Multi-body analysis of the main landing gear of Leonardo F48 UAV, file e384c430-1f77-d4b2-e053-9f05fe0a1d67
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14
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Technical report: Multi-body analysis of the nose landing gear of Leonardo F48 UAV, file e384c430-1f78-d4b2-e053-9f05fe0a1d67
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14
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On the role of large cross-sectional deformations in the nonlinear analysis of composite thin-walled structures, file e384c433-71d7-d4b2-e053-9f05fe0a1d67
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14
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Evaluation of transverse shear stresses in layered beams/plates/shells via stress recovery accounting for various CUF-based theories, file 2f28dc70-191a-4e7c-94d8-514d4702a4b2
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13
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Micropolar elasticity by unified theory, file e384c432-0a72-d4b2-e053-9f05fe0a1d67
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13
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Stress States in Highly Flexible Thin-Walled Composite Structures by Unified Shell Model, file e384c434-5f29-d4b2-e053-9f05fe0a1d67
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13
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Numerical vibration correlation technique for thin-walled composite beams under compression based on accurate refined finite element, file e384c434-9679-d4b2-e053-9f05fe0a1d67
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13
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Vibration Analysis of Curved Panel Subjected to Internal Pressure and Axial Compression, file b8fcab7e-3bc7-4811-bd32-d2ad3ce37d18
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12
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Preliminary technical report: Finite element structural analyses of the main landing gear of Leonardo F48 UAV, file e384c430-19a6-d4b2-e053-9f05fe0a1d67
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12
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Unified theory of structures based on micropolar elasticity, file e384c431-4c48-d4b2-e053-9f05fe0a1d67
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12
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Numerical simulation of deployable ultra-thin composite shell structures for space applications and comparison with experiments, file e384c434-ae0c-d4b2-e053-9f05fe0a1d67
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12
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Refined multilayered beam, plate and shell elements based on Jacobi polynomials, file 30bf2850-d3d6-42af-b966-855ef9d6eb9f
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11
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Preliminary technical report: Multi-body analysis of the main landing gear of Leonardo F48 UAV, file e384c430-1803-d4b2-e053-9f05fe0a1d67
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11
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Buckling test of stiffened panels: modeling and vibrational correlation testing, file 3515e9f5-f9be-4ffd-9b4e-9a47c3dceb4a
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10
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Stress and Failure Onset Analysis of Thin Composite Deployables by Global/Local Approach, file 700d5b2a-41fa-442a-b0cf-6b20f46916ed
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9
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Efficient CUF-based method for the vibrations of thin-walled open cross-section beams under compression, file e384c434-2c31-d4b2-e053-9f05fe0a1d67
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9
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Benchmarks for higher-order modes evaluation in the free vibration response of open thin-walled beams due to the cross-sectional deformations, file e384c434-324d-d4b2-e053-9f05fe0a1d67
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9
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Nonlinear analysis of thin-walled beams with highly deformable sections, file e384c432-46a2-d4b2-e053-9f05fe0a1d67
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6
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Use of Lagrange polynomials to build refined theories for laminated beams, plates and shells, file e384c434-4ac6-d4b2-e053-9f05fe0a1d67
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6
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Vibration Analysis of Curved Panel Subjected to Internal Pressure and Axial Compression, file 70c0b964-7830-4fdc-8c14-e90ea7d8cd74
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5
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Benchmarks for higher-order modes evaluation in the free vibration response of open thin-walled beams due to the cross-sectional deformations, file e384c433-b8d8-d4b2-e053-9f05fe0a1d67
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5
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Large deflection of composite beams by finite elements with node-dependent kinematics, file e384c434-319b-d4b2-e053-9f05fe0a1d67
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5
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Component-wise approach to reinforced concrete structures, file e384c434-4b0c-d4b2-e053-9f05fe0a1d67
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5
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Buckling test of stiffened panels: evaluation of post-buckling and failure by testing and layerwise models, file 1315b12e-3527-472e-add9-7333e712184d
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4
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Finite elements based on Jacobi shape functions for the analysis of beams, plates and shells, file 69236811-fdd2-4f74-a649-3e88c53a39ae
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4
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Virtual testing of folding and deployment of composite ultrathin tape spring hinges via unified 2D shell models, file 931f4c8d-791a-4a4a-8ee7-e36864d9e1ba
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4
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Frequency and mode change in the large deflection and post-buckling of compact and thin-walled beams, file e384c430-3297-d4b2-e053-9f05fe0a1d67
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4
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Evaluation of transverse shear stresses in layered beams/plates/shells via stress recovery accounting for various CUF-based theories, file 4a596020-24d0-4028-b67f-a4cb164b5ba6
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3
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Node-dependent kinematic models applied to reinforced concrete structures, file 931f43a9-e3d3-4a89-82d7-808a9aec7ba8
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3
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Unified theory of structures based on micropolar elasticity, file e384c431-6991-d4b2-e053-9f05fe0a1d67
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3
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Nonlinear analysis of thin-walled beams with highly deformable sections, file e384c432-46a1-d4b2-e053-9f05fe0a1d67
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3
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Vibration of metallic and composite shells in geometrical nonlinear equilibrium states, file e384c432-6570-d4b2-e053-9f05fe0a1d67
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3
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On the effectiveness of composite layers reinforcements on the static behaviour of damaged civil structures through unified formulation, file e384c433-fa4d-d4b2-e053-9f05fe0a1d67
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3
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Are There Cases in Which Classical Beam Theories Fail to Compute the Fundamental Frequency?, file ea865bd4-c8f9-4dce-9590-4cd3017a293a
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3
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Stress and Failure Onset Analysis of Thin Composite Deployables by Global/Local Approach, file 63308355-260b-4b87-9e84-f8e2ae76ba84
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2
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Multilayered Beam, Plate and Shell Theories with Interlaminar Variables and Lagrange Polynomials, file 6c3784fc-c205-44a0-90b6-6bdde41ec9b7
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2
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Evaluation of transverse shear stresses in layered beams/plates/shells via stress recovery accounting for various CUF-based theories, file a24bde48-ebf4-4d74-9a3a-5aefe9c49fda
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2
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A global/local element-wise approach for the buckling and post-buckling analysis of thin multilayered structures, file aa72d5ca-8358-44ca-84f1-58a3f1b9be3d
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2
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Refined multilayered beam, plate and shell elements based on Jacobi polynomials, file df1f777b-172f-44f8-9f6e-a05eb646399e
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2
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Effect of large displacements on the linearized vibration of composite beams, file e384c432-1450-d4b2-e053-9f05fe0a1d67
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2
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Popular benchmarks of nonlinear shell analysis solved by 1D and 2D CUF-based finite elements, file e384c432-337f-d4b2-e053-9f05fe0a1d67
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2
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Stress States in Highly Flexible Thin-Walled Composite Structures by Unified Shell Model, file e384c434-0fd5-d4b2-e053-9f05fe0a1d67
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2
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Static analysis of thin-walled beams accounting for nonlinearities, file e384c434-6587-d4b2-e053-9f05fe0a1d67
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2
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Vibration and buckling analysis of curved panel subjected to combined internal pressure and axial compression, file e384c434-8f68-d4b2-e053-9f05fe0a1d67
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2
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Unified plate finite elements for the large strain analysis of hyperelastic material structures, file 400ae23e-86de-4daa-a545-a9888a1a7c21
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1
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Evaluation of Various Geometrical Nonlinearities in the Response of Beams and Shells, file e384c431-39b4-d4b2-e053-9f05fe0a1d67
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1
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Optimized free-form surface modeling of point clouds from laser-based measurement, file e384c431-d487-d4b2-e053-9f05fe0a1d67
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1
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Evaluation of stress distributions in the geometrical nonlinear regime of functionally graded structures, file e384c431-f288-d4b2-e053-9f05fe0a1d67
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1
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Evaluation of geometrically nonlinear effects due to large cross-sectional deformations of compact and shell-like structures, file e384c431-f3f2-d4b2-e053-9f05fe0a1d67
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1
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Efficient CUF-based method for the vibrations of thin-walled open cross-section beams under compression, file e384c433-f5a3-d4b2-e053-9f05fe0a1d67
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1
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Unified plate finite elements for the large strain analysis of hyperelastic material structures, file f35d6823-9814-4f7d-910e-4058aa8eb013
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1
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| Totale |
1.185 |
Archivio Istituzionale della Ricerca