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Author ORCID Identifier

https://orcid.org/0009-0004-2737-3883

Date Available

8-5-2027

Year of Publication

2026

Document Type

Thesis

Degree Name

Masters in Aerospace Engineering

College

Engineering

Department/School/Program

Mechanical Engineering

Faculty

Xingsheng Sun

Jonathan Wenk

Abstract

Architected materials offer exceptional stiffness- and strength-to-weight performance, making them attractive for lightweight structural applications. However, predicting their mechanical response using conventional solid-element finite element analysis (FEA) is computationally expensive, limiting their use in early-stage design and large parameter studies. This work presents a computationally efficient framework combining bar-element finite element analysis with limit analysis (FEA-LA) to predict the elastic response, yield initiation, ultimate load, and collapse behavior of stretch-dominated lattice structures under quasi-static loading. The framework was verified against analytical solutions, compared with ANSYS solid-element simulations, and validated through uniaxial compression experiments on additively manufactured polymer octet-truss lattices. Calibration to experimental results enabled accurate prediction of stiffness, strength, and stress-strain behavior while reducing computational cost by approximately six to seven orders of magnitude compared with solid-element FEA. A parameter study investigated lattice-size effects on homogenized mechanical properties under uniaxial, biaxial, and triaxial compression, highlighting differences between load redistribution in the limit analysis formulation and the first-strut-yield criterion used in the finite element model. Finally, the FEA-LA framework was integrated with a Monte Carlo simulation to model manufacturing defects and reduce reliance on experimental calibration through uncertainty-based material parameters. The proposed framework provides an efficient tool for rapid mechanical characterization and design of stretch-dominated lattice materials.

Digital Object Identifier (DOI)

https://doi.org/10.13023/etd.2026.403

Archival?

Archival

1st Funding Information

NASA Kentucky Space Grant Consortium

Graduate Fellowship

80NSSC25M7090

2nd Funding Information

NASA Kentucky Space Grant Consortium

Research Experiences for Undergraduates

80NSSC20M0047

3rd Funding Information

University of Kentucky College of Engineering Department of Mechanical and Aerospace Engineering

College of Engineering Undergraduate Research Fellowship - Summer 2024

Available for download on Thursday, August 05, 2027

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