Date of Award
9-17-2015
Document Type
Thesis
Degree Name
Master of Science in Aeronautical Engineering
Department
Department of Aeronautics and Astronautics
First Advisor
Anthony N. Palazotto, PhD.
Abstract
A nonlinear analysis of a 3D icosahedron frame was conducted using ABAQUS, under a compressive load in which collapse occurs. The frame was created in SolidWorks using the material properties of the 3D plastic building material VeroBlue. Two considerations were made: the computational features of the frame, and the comparison between the experimental solution to the numerical solution. Two studies were also considered in this research: The first study was a comparison between the seven-inch and the four-inch icosahedron model with identical weight to buoyancy ratios; and the second study was a comparison between the seven-inch icosahedrons frame, with the experimental results of the data that was collected. The results of both studies are analyzed to compare against and verify the results of numerical computational model.
AFIT Designator
AFIT-ENY-MS-15-S-051
DTIC Accession Number
ADA621751
Recommended Citation
AlGhofaily, Mohammed, "Finite Element Analysis and Experimentation of an Icosahedron Frame under Compression" (2015). Theses and Dissertations. 1924.
https://scholar.afit.edu/etd/1924