journal article·2024-07Open access

Buckling and failure assessment of curved butt-joint stiffened thermoplastic composite panels with roller boundary conditions

Kevin van Dooren, Jan Waleson, Mark Chapman, Chiara Bisagni

Abstract

Two curved thermoplastic composite multi-stringer panels with roller boundary conditions are analysed and tested to investigate the buckling and failure behaviour. The panels are made of AS4D/PEKK-FC thermoplastic composite, have five stringers with an angled cap on the side and are joined to the skin with the short-fibre reinforced butt-joint technique. The panels have a roller attached to each loading edge, approximating simply-supported boundary conditions to apply compression and bending. One panel has an initial damage representing a barely visible impact damage in one of the stringer butt-joints, and one panel is in pristine condition. Finite element analyses are performed to predict the structural behaviour, and different approximations of the roller boundary conditions are compared. The analyses include material damage initiation and evolution. The out-of-plane displacement of the panels is measured by digital image correlation, and failure is captured with high-speed cameras. The panels fail in a sudden manner when the cap separates from the web, followed by web failure and skin-stringer separation in the butt-joint. The numerical analysis predicts the overall structural behaviour but cannot capture well the sudden panel collapse due to material damage.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Natural Fiber Reinforced Composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (43)

Show source-provided references
1. Skin-stringer separation in post-buckling of butt-joint stiffened thermoplastic composite panels10.1016/j.compstruct.2022.116294 ↗
2. Design, analysis and testing of thermoplastic welded stiffened panels to investigate skin-stringer separation in post-buckling10.1016/j.compositesb.2023.111033 ↗
3. Reeder · 1992
4. Modelling the crush behaviour of thermoplastic composites10.1016/j.compscitech.2016.07.015 ↗
5. Experimental and numerical evaluation of conduction welded thermoplastic composite joints10.1016/j.compstruct.2021.114964 ↗
6. On improving process efficiency and weld quality in ultrasonic welding of misaligned thermoplastic composite adherends10.1016/j.compstruct.2022.116342 ↗
7. Thermoplastic orthogrid fuselage shell
8. Development of innovative automated solutions for the assembly of multifunctional thermoplastic composite fuselage10.1007/s00170-021-07829-2 ↗
9. Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression10.1016/S1359-835X(99)00085-8 ↗
10. Experiment and analysis of hat-stringer-stiffened composite curved panels under axial compression10.1016/j.compstruct.2014.11.074 ↗
11. A post-buckling compressive failure analysis framework for composite stiffened panels considering intra-, inter-laminar damage and stiffener debonding10.1016/j.rinp.2019.102205 ↗
12. Kootte · 2023
13. Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel
14. Fatigue life and damage tolerance of postbuckled composite stiffened structures with indentation damage10.1177/0021998317715785 ↗
15. Panel stiffener debonding analysis using a shell/3D modeling technique10.1016/j.compscitech.2008.12.015 ↗
16. Single-stringer compression specimen for the assessment of damage tolerance of postbuckled structures10.2514/1.C031106 ↗
17. Progressive damage failure analysis of a multi-stringer post-buckled panel
18. Experimental study of post-buckled single-stringer composite specimens under fatigue loads with different load levels and load ratios10.1016/j.compositesb.2023.110606 ↗
19. Prediction of the postbuckling response of composite airframe panels including ply failure10.1016/j.engfracmech.2010.05.009 ↗
20. Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels10.1016/j.compscitech.2008.07.017 ↗
21. Experimental and numerical analysis for the post-buckling behavior of stiffened composite panels with impact damage10.1016/j.compstruct.2015.08.019 ↗
22. Damage and failure analysis of composite stiffened panels under low-velocity impact and compression after impact10.1016/j.compstruct.2020.113333 ↗
23. Damage sensitivity of axially loaded stringer-stiffened curved CFRP panels10.1016/j.compscitech.2009.10.013 ↗
24. J.W. van Ingen, J.E.A. Waleson, A. Offringa, M. Chapman, Double curved thermoplastic orthogrid rear fuselage shell, in: SAMPE Europe Conference. Nantes, France, 2019, pp. 1–10.
25. Kroll · 1953
26. Compression tests of sandwich panels with facings at different temperatures: Experimental deflection pattern found to correlate well with the assumed orthogonal sine-wave deflection pattern10.1007/BF02326724 ↗
27. Stiffener debonding mechanisms in post-buckled CFRP aerospace panels10.1016/j.compositesa.2004.12.003 ↗
28. Experimental investigation of the postbuckling response and collapse of a single-stringer specimen10.1016/j.compstruct.2013.09.018 ↗
29. Stiffened steel plates under compression and bending10.1016/S0143-974X(97)00058-8 ↗
30. Ultimate strength of stiffened plates with their stiffeners locally buckled in compression10.2534/jjasnaoe1968.1988.164_456 ↗
31. Experimental study of inelastic buckling strength and stiffness requirements for longitudinally stiffened panels10.1016/j.engstruct.2009.01.010 ↗
32. Stiffened aluminium panels subjected to axial compression10.1016/S0263-8231(01)00021-0 ↗
33. Experimental and numerical prediction of collapse of flatbar stiffeners in aluminum panels10.1061/(ASCE)0733-9445(2003)129:2(160) ↗
34. Edge-compression fixture for buckling studies of corrugated board panels10.1007/BF02319363 ↗
35. J.W. van Ingen, P. Lantermans, I. Lippers, Impact behaviour of a butt jointed thermoplastic stiffened skin panel, in: SAMPE 2012 International Symposium and Exhibition, 2012.
36. 2021
37. A fatigue failure criterion for fiber reinforced materials10.1177/002199837300700404 ↗
38. Progressive damage modeling in fiber-reinforced materials10.1016/j.compositesa.2007.01.017 ↗
39. Assessment of failure and cohesive zone length in co-consolidated hybrid C/PEKK butt joint10.1016/j.engstruct.2018.04.089 ↗
40. Multi-level experimental and numerical analysis of composite stiffener debonding. Part 1: Non-specific specimen level10.1016/j.compstruct.2009.04.001 ↗
41. Krueger · 2008
42. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus10.1016/0266-3538(96)00005-X ↗
43. Numerical simulation of mixed-mode progressive delamination in composite materials10.1177/0021998303034505 ↗