Modelling soft body impact on composite structures
Source abstract
Abstract
The paper describes recent progress on materials modelling and numerical simulation of soft body impact damage in fibre reinforced composite structures. The work is based on the application of finite element (FE) analysis codes to simulate composite shell structures under impact loads arising, for example, from bird strike on a wing leading edge. A composites ply damage mechanics model and interply delamination model have been implemented in an explicit FE code which is used to predict impact damage in shell structures. Soft body impactors such as gelatine (substitute bird) or ice (hailstones) are highly deformable on impact and flow over the structure spreading the impact load. They are modelled by a particle method in which the FE mesh is replaced by interacting particles. The failure models and code developments are applied to the numerical simulation of gas gun impact tests in which gelatine projectiles are fired at glass fabric/epoxy cylindrical shells.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · High-Velocity Impact and Material Behavior · Structural Response to Dynamic Loads
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (22)
Show source-provided references
1. Abrate · 1998
2. 1994 · vol. 9
3. Williams KV, Floyd AM, Vaziri R, Poursartip A. Numerical simulation of in-plane damage progression in laminated composite plates. 12th International Conference on Composite Materials (ICCM-12), 1999, Paris, France
4. Williams KV, Vaziri R. Finite element analysis of the impact response of CFRP composite plates. 10th International Conference on Composite Materials (ICCM-10), 1995, Whistler, Canada
5. A failure model for the analysis of thin woven glass composite structures under impact loadings10.1016/S0045-7949(00)00190-5 ↗
6. Inelastic strains and damage
7. Damage modelling of the elementary ply for laminated composites10.1016/0266-3538(92)90097-M ↗
8. Modelling fabric reinforced composites under impact loads10.1016/S1359-835X(00)00186-X ↗
9. PAM-SHOCK™/PAM-CRASH™ FE Code. Engineering Systems International, F-94578 Rungis Cedex, France
10. Kim H, Kedward KT. Experimental and numerical analysis correlation of hail ice impacting composite structures. 40th AIAA Structures, Structural Dynamics and Materials Conference, St Louis, 1999, AIAA-99-136610.2514/6.1999-1366 ↗
11. Iannucci L. Bird strike impact modelling. I. Mech. E. Seminar 1998, Foreign Object Impact and Energy Absorbing Structures, Inst. of Mech. Engineers, London
12. HICAS: High Velocity Impact of Composite Aircraft Structures. CEC DG XII BRITE-EURAM Project BE 96-4238, 1998
13. Interlaminar interface modelling for the prediction of delamination10.1016/0263-8223(92)90060-P ↗
14. Finite element methods and the progressive failure modelling of composite structures. CIMNE Barcelona
15. Computational methods for predicting impact damage in composite structures10.1016/S0266-3538(01)00111-7 ↗
16. Mixed-mode bending method for delamination testing
17. Smoothed particle hydrodynamics10.1146/annurev.aa.30.090192.002551 ↗
18. Numerical simulation of hypervelocity impact using the SPH option in PAM-SHOCK10.1016/S0734-743X(97)87503-3 ↗
19. Kamoulakos A, Groenenboom PHL. Moving form FE to SPH for space debris impact simulations––experience with PAM-SHOCK. Proceedings of European Conference on Spacecraft Structures: Materials and Mechanical Testing, Braunschweig, Germany, 1998
20. Hiermaier S, Thoma K. Computational simulation of high velocity impact situations using smoothed particle hydrodynamics. 9th DYMAT Technical Conference on Materials and Structural Modelling in Collision Research, TU Munich, Munich, Germany, 1995
21. Wilbeck JS. Impact behaviour of low strength projectiles. Air Force Materials Laboratory, Technical Report AFML-TR-77–134, 1977
22. Johnson AF, Holzapfel M. Computational methods for predicting impact damage in engineering composite structures. 5th World Congress on Computational Mechanics, WCCM V, Vienna, Austria, 2002