Analytical prediction of large mass impact damage in composite laminates
By R. Olsson. 2001
241 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Materials Chemistry, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/c43233da23695a156c2bfd4ae66f07ebbd84f3de
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Civil and Structural Engineering
- Pedro P. Camanho
- Cláudio S. Lopes
- Z. Sharif-Khodaei
- M. H. Aliabadi
- P. Maimí
- E. González
- Mazdak Ghajari
- L. Hounslow
In Materials Chemistry
- Z. Sharif-Khodaei
- Mazdak Ghajari
- M. H. Aliabadi
- Antonio Apicella
- P. Maimí
- Cláudio S. Lopes
- E. González
- Norbert Blanco
In Mechanics of Materials
- Pedro P. Camanho
- Cláudio S. Lopes
- P. Maimí
- Z. Sharif-Khodaei
- M. H. Aliabadi
- Mazdak Ghajari
- E. González
- L. Hounslow
Citations in the corpus
- Impact on composite structures (2004, background): “Comparisons between the theoretical threshold load and non-linear FE-analysis for various delamination locations were given by Olsson(2001).”
- Identification of impact force for smart composite stiffened panels (2013, methodology): “The delamination threshold force of the plate can be determined using the following relation (Olsson 2001): Fd = π √ 16D∗GIIc.”
- Numerical simulation of impact tests on GFRP composite laminates (2011, background): “To this aim, quite simple closed-form solutions [11], easy to use and effective, but restricted to simple impact cases due to the underlying simplifying assumptions [7,11,12], have been often employed.”
- Improvement of low-velocity impact and compression-after-impact performance by z-fibre pinning (2006, background): “The independency of sample size and boundary conditions was also studied numerically and experimentally in [18].”
- Effects of ply clustering in laminated composite plates under low-velocity impact loading (2011, methodology): “In addition, experimental data and finite element simulations indicate that the delamination threshold load is independent of the boundary conditions and of the in-plane size of the plate [24, 25, 36].”
- Determination of impact location on composite stiffened panels (2012, background): “For instance, for a transversely isotropic material (Olsson 2001): kH = 43 Q √ R (8) Q is the effective out-of-plane stiffness and given by: 1 Q = 1 Qzp + 1 Qzi (9) where Qz = Ez/(1− νrzνzr).”