Abstract
Air evacuation is crucial to achieve low porosity for vacuum-bag-only manufacturing of out-of-autoclave prepregs. In this paper, the air permeability of composite skins was evaluated for in-plane and transverse air evacuation. The air permeability and microstructure were evaluated for three common prepreg fabric architectures: unidirectional, plain weave, and 5 harness satin. Since prepreg permeability is anisotropic, a 3-D pressure gradient can arise in honeycomb skins. In-order to calculate the effective air permeability coefficients of honeycomb skins, the computational fluid dynamics software FLUENT was used to determine the 1-D pressure gradient and corresponding area normal to flow. The air permeability coefficients were correlated to the prepreg microstructure using micro-CT imaging. The results showed that the in-plane air permeability was higher for fabrics with larger visible dry tow areas. The transverse air permeability was higher for prepregs that formed connected macro-porosity networks after lay-up, compared to prepregs with isolated macro-pores. (C) 2013 Elsevier Ltd. All rights reserved.
Original language | English |
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Pages (from-to) | 179-191 |
Number of pages | 13 |
Journal | Composites Part A: Applied Science and Manufacturing |
Volume | 49 |
DOIs | |
Publication status | Published - Jun 2013 |
Keywords
- Air permeability
- A. Prepreg
- D. Radiography
- C. Computational modeling
- GAS-FLOW METHOD
- POROUS-MEDIA
- INPLANE PERMEABILITY
- SANDWICH STRUCTURES
- PERMEATION
- PRESSURE
- REINFORCEMENTS
- PREFORM