The impact performance of material‐extruded polymer components is strongly influenced by process‐dependent internal structure, making parameter selection critical for applications requiring improved damage tolerance. In this study, the Charpy impact strength of polylactic acid (PLA) parts fabricated by material extrusion was investigated using a three‐factor, three‐level full factorial design. The effects of layer height (0.1, 0.2, and 0.3 mm), raster angle (0°, 45°, and 90°), and infill geometry (triangle, octet, and gyroid) were evaluated across 27 unique processing conditions. By evaluating all parameter combinations using PLA at a fixed infill density of 20%, the full factorial design enabled determination of both the individual and interaction effects of the three parameters, rather than considering only isolated parameter trends. ISO 179‐compliant specimens were manufactured and tested under Charpy impact loading. Analysis of variance revealed that layer height was the primary factor influencing impact strength, followed by raster angle and its interaction with layer height, while infill geometry also made a significant contribution to the response. The highest impact strength of 10.59 ± 0.02 kJ/m
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was obtained at a layer height of 0.3 mm, a raster angle of 0°, and an octet infill geometry. In addition to inferential statistical analysis, an ordinary least squares quadratic response model was used to characterize the effect of layer height, indicating diminishing gains near the upper end of the investigated range. The results show that the impact resistance of material‐extruded PLA is governed by a coupled process–structure relationship and provide practical guidance for selecting printing conditions in applications requiring improved toughness and structural reliability.
This study systematically investigates and optimizes the influence of Fused Deposition Modeling (FDM) process parameters on the macroscopic tensile strength of polylactic acid (PLA) components. Addressing the need for predictable structural performance in 3D-printed parts, the novelty of this work lies in establishing...
Mehdi Moayyedian, M. Hedayati-Dezfooli, M. Fayed et al.· Journal of Manufacturing and...· 0 citations
Carbon fiber-reinforced thermoplastics processed by Material Extrusion (MEX) possess great potential for lightweight structural applications because to their superior mechanical properties and manufacturing flexibility. In this study, the impacts of six important MEX process parameters, layer height, extrusion temper...
A. Bint, Shamsher Singh, Anup Malik· Journal of Elastomers &...· 0 citations
This study investigates the optimization of Fused Deposition Modeling (FDM) parameters for Polyethylene Terephthalate Glycol (PETG) a material widely utilized in clinical and biomedical applications due to its favorable combination of lightweight properties, durability, and versatility. By applying a Grey-Taguchi metho...
Abera Anebo, Temesgen Abebe, D. Sinha· American Journal of Polymer...· 0 citations
This study investigates how geometric configurations and manufacturing parameters affect the crashworthiness performance of tubes printed by fused deposition modeling (FDM) using polymer filaments. Three distinct cross‐sectional geometries are evaluated using the standard polylactic acid (PLA), PLA PRO1, and carbon...
E. Albak, Ibrahim Berk Kucukgunduz, Murat Isik et al.· Polymer Composites· 0 citations
The combination of rigid Polylactic Acid (PLA) and elastic Thermoplastic Polyurethane (TPU) in a 3D-printed component may overcome individual polymer mechanical limitations. This multi-material concept is supported by the flexibility of the fused deposition modelling (FDM) technique of 3D printing. The present study ev...
Fellia Atma Garini, Salwa Fitria Rahimah, Keisha Euginia Gasperz et al.· International Conferences on...· 0 citations
This study investigates the manufacturing process, progressive damage behavior, and multiobjective structural optimization of 3D angle‐interlock woven composites (3DAWCs) fabricated via the resin transfer molding process. The 3DAWCs consist of T700‐12K carbon fiber preforms and an epoxy matrix system (LT‐5028A/B). A re...