Bull, 2012 - Google Patents
Numerical analysis and modelling of composite materialsBull, 2012
- Document ID
- 1078876528669090016
- Author
- Bull J
- Publication year
External Links
Snippet
Composite materials are increasingly used in many applications because they offer the engineer a range of advantages over traditional materials. They are often used in situations where a specified level of performance is required, but where the cost of testing the …
- 239000002131 composite material 0 title abstract description 76
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- 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
-
- 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
- G01N2203/0058—Kind of property studied
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Ostergaard et al. | Virtual testing of aircraft structures | |
Bühring et al. | Additive manufactured sandwich structures: Mechanical characterization and usage potential in small aircraft | |
Smojver et al. | Bird strike damage analysis in aircraft structures using Abaqus/Explicit and coupled Eulerian Lagrangian approach | |
Heimbs et al. | High‐velocity impact behaviour of prestressed composite plates under bird strike loading | |
Navarro et al. | Semi-continuous approach for the modeling of thin woven composite panels applied to oblique impacts on helicopter blades | |
Bull | Numerical analysis and modelling of composite materials | |
Sepe et al. | Numerical and experimental investigation on the structural behaviour of a horizontal stabilizer under critical aerodynamic loading conditions | |
Damghani et al. | Experimental and numerical study of hybrid (CFRP-GFRP) composite laminates containing circular cut-outs under shear loading | |
Beaumont | On the problems of cracking and the question of structural integrity of engineering composite materials | |
Gebhardt et al. | Low-velocity impact behavior of elliptic curved composite structures | |
Fleuret et al. | Complex wing spar design in carbon fiber reinforced composite for a light aerobatic aircraft | |
Chen et al. | Experimental and simulation investigation on BVID and CAI behaviors of CFRP laminates manufactured by RTM technology | |
Stickler | Composite materials for commercial transport-issues and future research direction | |
Marulo et al. | Numerical simulations and experimental experiences of impact on composite structures | |
Beaumont | Slow cracking in composite materials: Catastrophic fracture of composite structures | |
Cvitkovich et al. | Debonding in composite skin/stringer configurations under multi-axial loading | |
Castanié et al. | Multiaxial loading of aeronautic composite structures at intermediate scale: A review of VERTEX developments | |
Thakur et al. | Mode 1, Mode II, and Mixed Mode I/II Fracture Behavior of Laminated Structures | |
Johnson et al. | Design and testing of crashworthy aerospace composite components | |
Doubrava et al. | Application of bird-strike verified analysis for the design of fast helicopter composite Cowling | |
Feddal et al. | Delamination buckling of a laminated composite shell panel using cohesive zone modelling | |
Viitanen et al. | A Review of Aeronautical Fatigue Investigations in Finland April 2017-March 2019 | |
Doubrava et al. | Verification and numerical simulation of advanced composite inlet in compliance of airworthiness impact requirements | |
Kharat et al. | Stress analysis in composite pressure vessels-a review | |
Pineda et al. | Post-buckling Analysis of Curved Honeycomb Sandwhich Panels Containing Interfacial Disbonds |