CoChat
Sign Up
Cited by 44Mechanical Behavior of CompositesHigh-Velocity Impact and Material BehaviorCellular and Composite Structures

The DOI matches its Crossref record.

Soft body impact on laminated composite materials

Hou, J.P., Ruiz, C.·2007·Composites Part A: Applied Science and Manufacturing
DOI 10.1016/j.compositesa.2006.02.018
Open this paper in CoChat — free account

Overview

Integrity signals

Registry

Crossref · 10.1016/j.compositesa.2006.02.018

Cites

Statistics

Recomputing p-values needs the paper’s full text.

Verification

Claims the paper makes

We couldn’t retrieve this paper’s full text, so its claims and self-check weren’t run. The registry and citation checks still apply.

Citations

Cites

No references could be resolved yet.

Research works printed but not linked: 37

  1. Hughes DA. Analysis of bird impact on fan blade leading edge. DPhil thesis. Department of Engineering Science, Oxford University, 1992.
  2. Cantwell, 1991, The impact resistance of composite-materials—A review, Composites, 22, 347, 10.1016/0010-4361(91)90549-V · DOI
  3. Sun, 1990, Compos Sci Technol, 3, 327, 10.1016/0266-3538(90)90079-K · DOI
  4. Peck, 1991, The behaviour of delaminations in composite plates—Analytical and experimental results, J Compos Mater, 25, 907, 10.1177/002199839102500708 · DOI
  5. Liu, 1988, Impact-induced delamination—A view of bending stiffness mismatching, J Compos Mater, 22, 674, 10.1177/002199838802200706 · DOI
  6. Choi, 1991, A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact. Part 1. Experiments, J Compos Mater, 25, 992, 10.1177/002199839102500803 · DOI
  7. Choi, 1991, A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact. Part 2. Analysis, J Compos Mater, 25, 1012, 10.1177/002199839102500804 · DOI
  8. Wu HT, Springer GS. Impact damage of composites. In: Proceedings of the American society for composites, first technical conference, Dayton, October 1986. p. 346–51.
  9. Wang, 1994, Damage extension in carbon fibre/peek cross-ply laminates under low velocity impact, J Compos Mater, 28, 684, 10.1177/002199839402800801 · DOI
  10. Baucom, 2005, Low-velocity impact damage progression in woven E-glass composite systems, Composites A, 36, 658, 10.1016/j.compositesa.2004.07.008 · DOI
  11. Silva, 2005, Numerical simulation of ballistic impact on composite laminates, Int J Impact Eng, 31, 289, 10.1016/j.ijimpeng.2004.01.011 · DOI
  12. Kim, 2003, Experimental investigation of high velocity ice impacts on woven carbon/epoxy composite panels, Composites A, 34, 25, 10.1016/S1359-835X(02)00258-0 · DOI
  13. Johnson, 2003, Modelling soft body impact on composite structures, Compos Struct, 61, 103, 10.1016/S0263-8223(03)00033-3 · DOI
  14. McCarthy, 2004, Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates. Part 1. Material modelling, Appl Compos Mater, 11, 295, 10.1023/B:ACMA.0000037133.64496.13 · DOI
  15. McCarthy, 2004, Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates. Part 2. Modelling of impact with SPH bird model, Appl Compos Mater, 11, 317, 10.1023/B:ACMA.0000037134.93410.c0 · DOI
  16. Harding, 1983, A tensile testing technique for fibre-reinforced composites at impact rates of strain, J Mater Sci, 18, 1801, 10.1007/BF00542078 · DOI
  17. Harding, 1989, Characterisation of the impact strength of woven carbon-fibre epoxy laminates, Inst Phys Conf Ser, 102, 403
  18. Saka, 1990, A simple laminate theory approach to the prediction of the tensile impact strength of woven hybrid composites, Composites, 21, 439, 10.1016/0010-4361(90)90444-2 · DOI
  19. Xia, 1992, A transient stochastic failure model for unidirectional composites under impact, Compos Sci Technol, 43, 25, 10.1016/0266-3538(92)90130-U · DOI
  20. Xia, 1991, Analysis of damage in stress wave loaded unidirectional composites, Comput Struct, 8, 251, 10.1016/0045-7949(91)90103-S · DOI
  21. Li, 1991, Failure analysis of woven hybrid composites using a finite-element method, Compos Sci Technol, 41, 129, 10.1016/0266-3538(91)90024-J · DOI
  22. Chang, 1990, Characterization of impact damage in laminated composites, SAMPE J, 26, 18
  23. Aboudi, 1987, Transient waves in composite-materials, Wave Motion, 9, 141, 10.1016/0165-2125(87)90048-5 · DOI
  24. Xia, 1991, Transient shear deformation at interfaces of laminated beams, Int J Fract, 48, 205, 10.1007/BF00036632 · DOI
  25. McNiven, 1979, Propagation of transient waves in elastic laminated composites, Int J Solids Struct, 15, 271, 10.1016/0020-7683(79)90007-6 · DOI
  26. Witt, 1980, Dynamic response of laminated plates to random loading, Int J Solids Struct, 16, 231, 10.1016/0020-7683(80)90076-1 · DOI
  27. Mukunoki, 1980, Transient wave propagation normal to the layering of a finite layered medium, Int J Solids Struct, 16, 239, 10.1016/0020-7683(80)90077-3 · DOI
  28. Wu, 1989, Transient dynamic analysis of laminated composite plates subjected to transverse impact, Comput Struct, 31, 453, 10.1016/0045-7949(89)90393-3 · DOI
  29. Wu, 1988, Measurements of matrix cracking and delamination caused by impact on composite plates, J Compos Mater, 22, 518, 10.1177/002199838802200602 · DOI
  30. Wu, 1988, Impact induced stresses, strains, and delaminations in composite plates, J Compos Mater, 22, 533, 10.1177/002199838802200603 · DOI
  31. Aggour, 1988, Finite-element analysis of a laminated composite plate subjected to circularly distributed central impact loading, Comput Struct, 28, 729, 10.1016/0045-7949(88)90412-9 · DOI
  32. Sun, 1989, Investigation of laminated composite plates under impact dynamic loading using a 3-dimensional hybrid stress finite-element method, Comput Struct, 33, 879, 10.1016/0045-7949(89)90263-0 · DOI
  33. Hughes DA. Experimental results of the leading edge bird impact tests. Rolls-Royce Oxford U.T.C. Report No. 15, 1991.
  34. Wilbeck, 1981, The development of a substitute bird model, J Eng Power, 103, 725, 10.1115/1.3230795 · DOI
  35. Takeda, 1981, Studies of impacted glass fibre-reinforced composite laminates, SAMPE Quart, 9
  36. Liu, 1988, Impact-induced delamination—a view of bending stiffness mismatching, J Compos Mater, 22, 674, 10.1177/002199838802200706 · DOI
  37. Davies AGO, Zhang X, Hitchings D. Modelling impact damage in laminated composites. In: Proceedings NAFEMS world congress, Stuttgart, April 1997. p. 1216–31.

Cited by

Sorted by citations

Metadata

Authors
Hou, J. P., & Ruiz, C.
Affiliations
  • Zhengzhou University (CN)
  • University of Oxford (GB)
Corresponding author
Hou, J.P.
ORCID
Venue
Composites Part A: Applied Science and Manufacturing
Publisher
Elsevier BV
Published
2007-02
Volume
38
Issue
2
Pages
505-515
ISSN
1359-835X (ISSN-L)
DOI
10.1016/j.compositesa.2006.02.018
OpenAlex
W2046328766
Cited by
44
References
0
Citations by year
2026: 1 · 2025: 1 · 2023: 3 · 2021: 2 · 2020: 4 · 2019: 5 · 2018: 1 · 2016: 4 · 2015: 5 · 2014: 3 · 2012: 3
FWCI
0.00
Type
journal article
Language
en
Open access
closed
Licence
www.elsevier.com/tdm/userlicense/1.0/ (tdm)
Locations
Composites Part A Applied Science and Manufacturing (publishedVersion)
Topics
  • Physical Sciences › Engineering › Mechanics of Materials › Mechanical Behavior of Composites
  • Physical Sciences › Engineering › Mechanics of Materials › High-Velocity Impact and Material Behavior
  • Physical Sciences › Engineering › Mechanical Engineering › Cellular and Composite Structures
Keywords
soft body impact, composite laminates, carbon fiber reinforced polymer, bird strikes, impact damage modes, ultrasonic C-scan, high-velocity impact

About these checks

Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

Statistics and arithmetic are recomputed, not judged.

Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.

What counts as a claim ›How we measure confidence ›How we check this ›

Are you an author, or do you see a problem with this page? Request a review