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editor-in-chief

Editors-in-Chief

Prof. Sivanesan Subramanian

Anna University, India

 

Prof. Hassan Karimi-Maleh

University of Electronic Science
and Technology of China (UESTC)

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2578-2010 (Online)

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Home > Archives > Vol 7, No 2 (Published) > Original Research Article
ACE-1875

Published

2024-04-15

Issue

Vol 7, No 2 (Published)

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Original Research Article

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Copyright (c) 2024 S Raja

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How to Cite

Raja, S., Al-Tmimi, H. M., Ghadir, G. K., Mustafa, M. A., Alani, Z. K., Rusho, M. A., & Rajeswari, N. (2024). An analysis of polymer material selection and design optimization to improve Structural Integrity in 3D printed aerospace components. Applied Chemical Engineering, 7(2), 1875. https://doi.org/10.59429/ace.v7i2.1875
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An analysis of polymer material selection and design optimization to improve Structural Integrity in 3D printed aerospace components

S Raja

Center of Additive Manufacturing, Chennai Institute of Technology

Hayder Musaad Al-Tmimi

Department of Pathological Analysis, College of Health Medical Techniques, Al-Bayan University

Ghadir Kamil Ghadir

College of Pharmacy, Al-Farahidi University

Mohammed Ahmed Mustafa

Department of Medical Laboratory Technology, University of Imam Jaafar AL-Sadiq

Zaid Khalid Alani

Department of Pathological Analysis, College of Health Medical Techniques, Al-Bayan University

Maher Ali Rusho

Lockheed Martin Performance-Based Master of Engineering in Engineering Management (ME-EM) Degree Program, University of Colorado Boulder

N. Rajeswari

Department of Mechanical Engineering, Surya Engineering College


DOI: https://doi.org/10.59429/ace.v7i2.1875


Keywords: material selection; design optimization; structural integrity; 3D Printing; aerospace


Abstract

This paper presents an analysis of material selection and design optimization techniques to enhance the structural integrity of 3D printed aerospace components. The study highlights the importance of considering material characteristics and design factors such as shape, orientation, and support structures in order to achieve reliable and high-performance components. Various materials, including metals and polymers, commonly used in aerospace applications are evaluated, along with their properties and limitations in the context of 3D printing. Furthermore, the impact of different printing parameters on the structural integrity of the components is discussed. The study identifies optimization strategies such as topology optimization, lattice structures, and infill patterns, which can significantly improve the strength and durability of 3D printed parts. The results demonstrate the potential of these techniques to optimize the design and material selection of aerospace components, leading to lighter, more efficient, and reliable parts for air and space vehicles.


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