Serra et al., 2017 - Google Patents
Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 2: Load envelopes for the assessment of …Serra et al., 2017
View PDF- Document ID
- 3567825808726633280
- Author
- Serra J
- Pierré J
- Passieux J
- Périé J
- Bouvet C
- Castanié B
- Petiot C
- Publication year
- Publication venue
- Composite Structures
External Links
Snippet
One of the important issues in the certification of composite aeronautical structures is large notches. In this paper, tests are carried out on technological specimens under tensile, shear and combined loadings using the VERTEX test rig presented in the first part of this …
- 239000002131 composite material 0 title abstract description 47
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/026—Specifications of the specimen
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5086—Mechanical design, e.g. parametric or variational design
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0058—Kind of property studied
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges, air-craft wings
- G01M5/0041—Investigating the elasticity of structures, e.g. deflection of bridges, air-craft wings by determining deflection or stress
- G01M5/005—Investigating the elasticity of structures, e.g. deflection of bridges, air-craft wings by determining deflection or stress by means of external apparatus, e.g. test benches or portable test systems
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Serra et al. | Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 2: Load envelopes for the assessment of panels with large notches | |
| Serra et al. | Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 1: Experimental setup, FE-DIC instrumentation and procedures | |
| Zhao et al. | Modeling the transverse tensile and compressive failure behavior of triaxially braided composites | |
| Nikishkov et al. | Progressive fatigue damage simulation method for composites | |
| Lopes et al. | Multiscale virtual testing: the roadmap to efficient design of composites for damage resistance and tolerance | |
| Zarouchas et al. | Investigations on the mechanical behavior of a wind rotor blade subcomponent | |
| Rozylo et al. | Stability and failure analysis of compressed thin-walled composite structures with central cut-out, using three advanced independent damage models | |
| Krueger et al. | Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin-stiffener debonding | |
| Qian et al. | Experimental and numerical study on shear-punch test of 6060 T6 extruded aluminum profile | |
| McElroy | Use of an enriched shell finite element to simulate delamination-migration in a composite laminate | |
| Akterskaia et al. | Efficient progressive failure analysis of multi-stringer stiffened composite panels through a two-way loose coupling global-local approach | |
| Abdollahzadeh et al. | Experimental and numerical investigation on large deformation reconstruction of thin laminated composite structures using inverse finite element method | |
| Al-Azzawi et al. | Buckling and postbuckling behaviour of Glare laminates containing splices and doublers. Part 2: Numerical modelling | |
| McQuigg | Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesheets | |
| Li et al. | Simplified analytical model and balanced design approach for light-weight wood-based structural panel in bending | |
| Masood et al. | Experimental and finite element numerical studies on the post-buckling behavior of composite stiffened panels | |
| Damghani et al. | Experimental and numerical study of hybrid (CFRP-GFRP) composite laminates containing circular cut-outs under shear loading | |
| Laustsen et al. | Development of a high‐fidelity experimental substructure test rig for grid‐scored Sandwich panels in wind turbine blades | |
| Wu et al. | Experimental behavior and shear bearing capacity simulation of stiffened composite panels subjected to invisible damage impact | |
| McQuigg et al. | Compression after impact experiments on thin face sheet honeycomb core sandwich panels | |
| Ginot et al. | Local buckling on large sandwich panels applied to light aviation: Experimental and computation dialogue | |
| Farrokhabadi et al. | Assessment of delamination growth due to matrix cracking in hybrid Glass-Kevlar composite laminates using experimental, numerical and analytical methods | |
| Hobbiebrunken et al. | Influence of non-uniform fiber arrangement on microscopic stress and failure initiation in thermally and transversely loaded CF/epoxy laminated composites | |
| McQuigg et al. | Compression after impact on honeycomb core sandwich panels with thin facesheets, part 1: experiments | |
| Justusson et al. | A technical approach for assessing progressive damage and failure analysis methods for structural performance |