Sustainable Aerospace Composites: Enhancing Mechanical Performance of FFF-Printed Onyx Through Fibre Optimization
Abstract Carbon fibre composites, known for their high strength-to-weight ratio, are extensively used in critical aerospace components. However, traditional manufacturing methods are time-intensive, costly, and resource-heavy. Fused Filament Fabrication (FFF), a material extrusion-based additive manufacturing technique, offers a sustainable alternative, enabling complex geometries with minimal waste. Despite its advantages, FFF-printed parts made from standard thermoplastics often lack the mechanical strength needed for high-stress applications. This study investigates the mechanical performance of nylon-short carbon fibre (Onyx) and carbon fibre-reinforced composites with different lay-up orientations. Composites with [0,90]s and [0,45,90,−45]s orientations were compared to non-oriented samples which showcased significant improvements in flexural and comparable tensile strength respectively. Scanning electron microscopy revealed that the fibre alignment delayed crack propagation and enhanced durability, with fibre pull-out as the primary failure mechanism. These findings demonstrate that optimizing fibre orientation during FFF can significantly improve composite performance, offering a sustainable pathway for high-performance applications in aerospace and automotive industries where strength, efficiency, and sustainability are paramount.
Authors
- Meysam Nasr Azadani
- Karthikeyan Ramachandran (ORCID: https://orcid.org/0000-0003-2246-7309)
- Vishaal Harikrishna Kumar (ORCID: https://orcid.org/0009-0001-4386-1375)
- Jayesh Shanthi Bhavan (ORCID: https://orcid.org/0000-0003-2378-7478)
- Constance L. Gnanasagaran (ORCID: https://orcid.org/0000-0002-9982-8216)
Institutions
- Indian Institute of Technology Indore (IN)
- Coventry University (GB)
Publication Details
- Published
- 2025-05-05
- DOI
- https://doi.org/10.1115/ssdm2025-151334
- Primary Topic
- Spacecraft Design and Technology
- Type
- article
- Field-Weighted Citation Impact
- 0.00