Impact on composite structures
By G. Davies, R. Olsson. Aeronautical Journal, 2004
733 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/bf14fc5c8be56f8733a1b699934e5f85387a7888
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
- C. Bouvet
- Pedro P. Camanho
- Cláudio S. Lopes
- Brian G. Falzon
- Z. Sharif-Khodaei
- M. H. Aliabadi
- S. Rivallant
- P. Maimí
In Mechanics of Materials
- C. Bouvet
- Pedro P. Camanho
- Brian G. Falzon
- S. Rivallant
- N. Hongkarnjanakul
- Cláudio S. Lopes
- P. Maimí
- S. Hallett
Citations in the corpus
- Improvement of low-velocity impact and compression-after-impact performance by z-fibre pinning (2006, methodology): “4% is currently used for aircraft compression panels while the undamaged material should be capable of strain limits of 1% or higher [1-5].”
- Electrospun nanofibers as reinforcement for composite laminates materials – a review (2017, unknown): “Impacts on composite structures may induce delamination cones through the thickness, irreversibly damaging the structure [114].”
- Lightweight sandwich structures for marine applications: a review (2021, background): “Contact force evaluation history in the elastic phase (if that the structure stiffness is known) [68, 69]”
- Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements (2013, background): “This damage is particularly dangerous because it drastically reduces the residual mechanical characteristics of the structure, and, at the same time, can leave a very small visible mark on the impacted surface [1], which makes it difficult to detect.”
- Delamination threshold load for dynamic impact on plates (2006, background): “9 68 46 Morita et al. (1997) AS4/PEEK (03/453/903/ 453)s 3.”
- Determination of impact location on composite stiffened panels (2012, background): “The latter can be categorized as large mass impacts for which the impact time is long enough that the behaviour of the structure is similar to its response under quasi-static loading and local effects such as indentation are small (Davies and Olsson 2004).”
- Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI): Experimental and numerical study (2018, background): “As the delamination area increases and surpasses a critical size as a result of increasing impact energy, the CAI strength drops significantly and then tends to level off, where it is equivalent to a complete perforation of the same size as the delaminated region [12,20,21].”
- Numerical simulation of impact tests on GFRP composite laminates (2011, background): “Although these materials offer very attractive properties, their application is often restricted by their vulnerability to transverse impact [1], forcing the adoption of large safety factors and resulting in significantly over-designed structures.”
- Plastic Deformation, Failure and Energy Absorption of Sandwich Structures with Metallic Cellular Cores (2010, background): “The parameters governing the indentation response of sandwich panels may include: the material properties and geometry of the face-sheet and core, shape of projectile, boundary conditions and impact velocity [51].”
- Low velocity impact modelling in laminate composite panels with discrete interface elements (2009, methodology): “Before concluding from this bibliography, which is of course not exhaustive, the authors invite the interest readers to consult review papers of Abrate (1998) or Davies and Olsson (2004).”
- Impact and compression after impact experimental study of a composite laminate with a cork thermal shield (2007, unknown): “These curves, representative of all performed impact tests, are very classic in the literature [7,9].”
- Recent Advances in Active Infrared Thermography for Non-Destructive Testing of Aerospace Components (2018, background): “These types of material defects may occur at any stage of the component’s cycle life, from manufacturing to in-service and maintenance operations [6].”
- Effects of ply clustering in laminated composite plates under low-velocity impact loading (2011, methodology): “The stiffnesses kbs and km can be obtained experimentally, by using numerical methods, or analytically in cases with simple geometries [5].”
- Unscented Kalman filtering for nonlinear structural dynamics (2007, background): “This aspect can be partially dealt with by adopting the iterated extended Kalman filter (IEKF) [9,33].”