Abstract
This paper reports on initial investigations into the manufacturing and testing of Stiffened Carbon Fibre Composite Panels for buckling and postbuckling strength. Five panels were manufactured using different manufacturing techniques and a full description of these panels is given. All panels were tested to failure in an INSTRON compression testing machine. Buckling mode shapes were observed through the use of the Shadow Moire Fringe technique and strain measurements were obtained using resistive strain gauges. Linear finite element analysis was also carried out to compare predicted buckling loads with experimental results.
| Original language | English |
|---|---|
| Title of host publication | EventAdvanced Composites '93: International Conference on Advanced Composite Materials |
| Publisher | Publ by Minerals, Metals & Materials Soc (TMS) |
| Number of pages | 8 |
| Publication status | Published - 1993 |
Bibliographical note
Composites '93: International Conference on Advanced Composite MaterialsWollongong, Australia
15 - 19 Feb 1993
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 9 Industry, Innovation, and Infrastructure
Keywords
- Airframes Buckling Composite structures Compression testing Failure (mechanical) Finite element method Mechanical testing Moire fringes Strain gages Strength of materials Structural analysis Structural panels Manufacturing method effects Postbuckling strength Thin skinned carbon fibre composite panels Carbon fiber reinforced plastics
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