| Nome |
# |
|
Fibre optics health monitoring for aeronautical applications, file e0c31c0d-e589-4599-e053-1705fe0aef77
|
226
|
|
Quasi-static and impact behaviour of foam-filled graded auxetic panel, file 6d8633a3-0508-4300-a685-056c2d2b039e
|
198
|
|
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft, file e0c31c0d-1c06-4599-e053-1705fe0aef77
|
179
|
|
Impact response of composite energy absorbers based on foam-filled metallic and polymeric auxetic frames, file 2742f711-93eb-4be7-b346-50de11524fc0
|
153
|
|
Numerical And Experimental Crushing Behaviour Investigation Of EBM Printed Auxetic Chiral Lattices, file e0c31c0e-5412-4599-e053-1705fe0aef77
|
143
|
|
Chiral topologies for composite morphing structures - Part II: Novel configurations and technological processes, file e0c31c0e-4fff-4599-e053-1705fe0aef77
|
142
|
|
Reliability of strain monitoring of composite structures via the use of optical fiber ribbon tapes for structural health monitoring purposes, file e0c31c0d-a20e-4599-e053-1705fe0aef77
|
132
|
|
Foam-filled energy absorbers with auxetic behaviour for localized impacts, file e0c31c0f-75b7-4599-e053-1705fe0aef77
|
128
|
|
Investigation of Ceramics Matrix Composite Material Suitability for an Aeronautical Application, file 203038d3-5ea9-4198-b832-14e92c085daa
|
94
|
|
A bi-phasic modelling approach for interlaminar and intralaminar damage in the matrix of composite laminates, file e0c31c0e-eaaf-4599-e053-1705fe0aef77
|
89
|
|
Design and manufacturing of skins based on composite corrugated laminates for morphing aerodynamic surfaces, file e0c31c0e-2aea-4599-e053-1705fe0aef77
|
78
|
|
Chiral topologies for composite morphing structures - Part I: Development of a chiral rib for deformable airfoils, file e0c31c0e-5008-4599-e053-1705fe0aef77
|
77
|
|
Efficient Modelling of Forces and Local Strain Evolution During Delamination of Composite Laminates, file e0c31c0e-3fbd-4599-e053-1705fe0aef77
|
70
|
|
Compression Behavior of EBM Printed Auxetic Chiral Structures, file e0c31c12-8bc6-4599-e053-1705fe0aef77
|
64
|
|
Approaches for Numerical Analysis and Experimental Monitoring of Manufacturing Process and Damage Evolution in Carbon/Titanium Hybrid Structures, file e0c31c0e-6a11-4599-e053-1705fe0aef77
|
56
|
|
Experimental Identification of Frictional Effects on Interlaminar Toughness of Composite Laminates in 4ENF Test, file a83a9e64-105d-4227-bb26-8ec23adb3114
|
52
|
|
Design of a Morphing Actuated Aileron with Chiral Composite Internal Structure, file e0c31c0d-beb5-4599-e053-1705fe0aef77
|
50
|
|
Flexible joints based on corrugated composite laminates: numerical development and manufacturing, file e0c31c12-597d-4599-e053-1705fe0aef77
|
47
|
|
Modelling and Monitoring the Response of Bonded Composite/Metallic Structures During Manufacturing Process and Damage Evolution, file e0c31c0c-a900-4599-e053-1705fe0aef77
|
46
|
|
Numerical and Experimental Methods for the Identification of Interlaminar Properties in LSI Manufactured C/SiC Composite, file f53e7ab9-34f5-4850-83a3-7de56fb4b113
|
44
|
|
Characterization and numerical interpretation of non-linear tensile response in UHTCMC, file 228b015c-cd5f-482a-816f-e2ad271ffd64
|
41
|
|
A meso-scale model of progressive damage and failure in LSI-produced ceramic matrix composites for aerospace applications, file a4bd2982-6942-40c3-be8a-4f8dada8cc7f
|
24
|
|
Development and manufacturing of flexible joints based on corrugated composite laminates, file cda502c4-a068-4870-89ea-d67e98b0fba2
|
16
|
|
A model for damage and failure of carbon-carbon composites: development and identification through Gaussian process regression, file 890449db-af51-48e5-b1f1-125bd529f6b8
|
14
|
|
Effect of Hygrothermal Ageing on Optical Fibersensorized Composite Materials, file e0c31c11-7ba0-4599-e053-1705fe0aef77
|
12
|
|
Interlaminar Response of LSI-Produced C/SiC Ceramic Matrix Composites: Experiments and Modelling, file 277a2153-b027-43a0-bc91-217b8cbc3ff3
|
11
|
|
Feasibility of a Morphing Rocket Nozzle for Thrust Vector Control based on Corrugated Composite Laminates, file 89270549-d519-4f4d-9185-606acc6317eb
|
9
|
|
Impact Response of Monolithic and Laminated Polycarbonate Panels: An Experimental and Numerical Investigation, file 54d14499-adbb-4025-8be8-55042c3924b9
|
7
|
|
Chiral topologies for composite morphing structures - Part II: Novel configurations and technological processes, file e0c31c08-6290-4599-e053-1705fe0aef77
|
7
|
|
Meso-Scale Models to Analyse the Interactions of Damage Modes in Composites Laminates, file 4d23ff74-f861-4818-9b75-0d936e3ee414
|
6
|
|
Chiral topologies for composite morphing structures - Part I: Development of a chiral rib for deformable airfoils, file e0c31c08-5d59-4599-e053-1705fe0aef77
|
6
|
|
A bi-phasic modelling approach for interlaminar and intralaminar damage in the matrix of composite laminates, file e0c31c0e-f381-4599-e053-1705fe0aef77
|
6
|
|
Thermomechanical response of out-of-autoclave infused carbon-phenolic laminates for rocket engine applications subjected to surface ablation, file 3c1bdcbd-25e6-4953-ad1e-d51951b406c7
|
5
|
|
Development of an Additive Manufactured Fitting Sensorized with Optical Fibres for Load Recognition, file 6ec1e5d8-2fc5-47f0-9129-bea8cb67e110
|
5
|
|
Analysis of residual stresses and interface damage propagation in hybrid composite/metallic elements monitored through optical fiber sensors, file e0c31c12-805f-4599-e053-1705fe0aef77
|
5
|
|
Thermomechanical response of out-of-autoclave infused carbon-phenolic laminates for rocket engine applications subjected to surface ablation, file 9b83ad52-c64b-4fe3-9c00-fef9a726e2de
|
4
|
|
Design and manufacturing of skins based on composite corrugated laminates for morphing aerodynamic surfaces, file e0c31c0a-735a-4599-e053-1705fe0aef77
|
4
|
|
Actuated Composite Corrugated Laminates for Morphing Aerodynamic Surfaces, file e0c31c0e-b828-4599-e053-1705fe0aef77
|
4
|
|
Numerical and Experimental Methods for the Identification of Interlaminar Properties in LSI Manufactured C/SiC Composite, file 1489a26c-8f79-4bc4-aa8c-c4a2b6ec8665
|
3
|
|
Implementation of a Damage Model for Tension and Bending of Ceramic Matrix Composites with Statistical Distribution of Proprerties, file 857c6874-c4b6-4c62-b303-d730b8ba18c7
|
3
|
|
Efficient Modelling of Forces and Local Strain Evolution During Delamination of Composite Laminates, file e0c31c08-2469-4599-e053-1705fe0aef77
|
3
|
|
Design of a Morphing Actuated Aileron with Chiral Composite Internal Structure, file e0c31c08-280e-4599-e053-1705fe0aef77
|
3
|
|
Development of a Numerical Mesoscale Material Model for Short Fibre-Reinforced Ceramics Matrix Composites, file e0c31c08-7b85-4599-e053-1705fe0aef77
|
3
|
|
Design of Health and Usage Monitoring Systems Based on Optical Fibers for Composite Wing Spars, file e0c31c08-d5ad-4599-e053-1705fe0aef77
|
3
|
|
Experimental and Numerical Investigation of Damage Evolution in Curved Composite Laminates, file e0c31c0e-69ee-4599-e053-1705fe0aef77
|
3
|
|
A bi-phasic numerical approach for non-linear response and stiffness recovery related to residual thermal stress in UHTCMCs, file 0ba5b607-fa2e-401d-9f00-0587ce6c662a
|
2
|
|
Design of a Morphing Airfoil with Composite Chiral Structure, file e0c31c08-73c7-4599-e053-1705fe0aef77
|
2
|
|
Design of a Motorcycle Composite Swing-Arm by Means of Multi-Objective Optimisation, file e0c31c08-76b7-4599-e053-1705fe0aef77
|
2
|
|
Direct Search of Feasible Region and Application to a Crashworthy Helicopter Seat, file e0c31c08-76ba-4599-e053-1705fe0aef77
|
2
|
|
Reliability of strain monitoring of composite structures via the use of optical fiber ribbon tapes for structural health monitoring purposes, file e0c31c08-912d-4599-e053-1705fe0aef77
|
2
|
|
Composite Corrugated Laminates for Morphing Applications, file e0c31c0b-4d16-4599-e053-1705fe0aef77
|
2
|
|
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft, file e0c31c0b-5645-4599-e053-1705fe0aef77
|
2
|
|
Characterization and numerical interpretation of non-linear tensile response in UHTCMC, file fd7b98a7-4e37-4fe2-a1e0-cf4d4d13dcc3
|
2
|
|
Identification of Material Parameters for Modelling Delamination in the Presence of Fibre Bridging, file e0c31c08-76d1-4599-e053-1705fe0aef77
|
1
|
|
An Efficient Approach for Modeling Interlaminar Damage in Composite Laminates with Explicit Finite Element Codes, file e0c31c08-fb84-4599-e053-1705fe0aef77
|
1
|
|
Morphing Composite Structures for Adaptive High Lift Devices, file e0c31c09-7f10-4599-e053-1705fe0aef77
|
1
|
|
Strain field reconstruction on composite spars based on the identification of equivalent load conditions, file e0c31c0a-c8ca-4599-e053-1705fe0aef77
|
1
|
|
Interlaminar Damage Detection in Composite Elements by Means of Optical Fibre Sensors, file e0c31c0b-267c-4599-e053-1705fe0aef77
|
1
|
|
Composites Interlaminar Toughening Techniques by Means of Interleaved Nanofiber Veils: Experimental Evaluation, file e0c31c0b-3f61-4599-e053-1705fe0aef77
|
1
|
|
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project, file e0c31c0c-75e9-4599-e053-1705fe0aef77
|
1
|
|
Modelling and Monitoring the Response of Bonded Composite/Metallic Structures During Manufacturing Process and Damage Evolution, file e0c31c0c-a901-4599-e053-1705fe0aef77
|
1
|
|
Fibre optics health monitoring for aeronautical applications, file e0c31c0d-e591-4599-e053-1705fe0aef77
|
1
|
| Totale |
2.300 |