Koh et al., 2013 - Google Patents
Experimental assessment of the damage tolerance of z-pinned T-stiffened composite panelsKoh et al., 2013
View HTML- Document ID
- 6262766710915951296
- Author
- Koh T
- Isa M
- Feih S
- Mouritz A
- Publication year
- Publication venue
- Composites Part B: Engineering
External Links
Snippet
Stiffened composite panels used in aircraft, buildings and other light-weight structural applications are susceptible to unstable bond-line cracking that results in poor damage tolerant properties. This paper presents an experimental study into the improvement to the …
- 239000002131 composite material 0 title abstract description 50
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Koh et al. | Experimental assessment of the damage tolerance of z-pinned T-stiffened composite panels | |
| Karaboğa et al. | Mechanical response of carbon fiber reinforced epoxy composite parts joined with varying bonding techniques for aerospace applications | |
| Koh et al. | Experimental determination of the structural properties and strengthening mechanisms of z-pinned composite T-joints | |
| Wu et al. | Comparison on damage tolerance of scarf and stepped-lap bonded composite joints under quasi-static loading | |
| Nanayakkara et al. | Improving the fracture resistance of sandwich composite T-joints by z-pinning | |
| Bianchi et al. | Finite element modelling of z-pinned composite T-joints | |
| Liu et al. | The impact damage and residual load capacity of composite stepped bonding repairs and joints | |
| Campilho et al. | Tensile behaviour of three-dimensional carbon-epoxy adhesively bonded single-and double-strap repairs | |
| Koh et al. | Strengthening mechanics of thin and thick composite T-joints reinforced with z-pins | |
| Camanho et al. | Hybrid titanium–CFRP laminates for high-performance bolted joints | |
| Löbel et al. | A hybrid bondline concept for bonded composite joints | |
| Atas et al. | An experimental investigation on the low velocity impact response of composite plates repaired by VARIM and hand lay-up processes | |
| Isa et al. | Compression fatigue properties of z-pinned quasi-isotropic carbon/epoxy laminate with barely visible impact damage | |
| Truong et al. | Cohesive zone method for failure analysis of scarf patch-repaired composite laminates under bending load | |
| Shah et al. | Determination of mode I & II strain energy release rates in composite foam core sandwiches. An experimental study of the composite foam core interfacial fracture resistance | |
| Greenhalgh et al. | Evaluation of toughening concepts at structural features in CFRP—Part I: Stiffener pull-off | |
| Guo et al. | Numerical analysis and experiment of sandwich T-joint structure reinforced by composite fasteners | |
| Gamdani et al. | Fatigue behavior of hybrid multi-bolted-bonded single-lap joints in woven composite plates | |
| Ghasemnejad et al. | Effect of delamination failure in crashworthiness analysis of hybrid composite box structures | |
| Tzetzis et al. | Experimental and finite element analysis on the performance of vacuum-assisted resin infused single scarf repairs | |
| Liu et al. | Study on impact damage mechanisms and TAI capacity for the composite scarf repair of the primary load-bearing level | |
| Mouritz et al. | Tension fatigue of fibre-dominated and matrix-dominated laminates reinforced with z-pins | |
| Shah et al. | Effect of adhesive thickness on the Mode I and II strain energy release rates. Comparative study between different approaches for the calculation of Mode I & II SERR's | |
| Ravindran et al. | Design considerations in the strengthening of composite lap joints using metal z-pins | |
| Ji et al. | Fatigue characteristics of stainless steel pin-reinforced composite hat joints |