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Conceptual Fuselage Design with Direct CAD Modeling


Abstract In today’s day and age, the use of automated technology is becoming increasingly prevalent. Throughout the aerospace industry, we see the use of automated systems in manufacturing, testing, and, progressively, in design. This thesis focuses on the idea of automated structural design that can be directly coupled with parametric Computer-Aided Drafting (CAD) and used to support aircraft conceptual design. This idea has been around for many years; however, with the advancement of CAD technology, it is becoming more realistic. Having the ability to input design parameters, analyze the structure, and produce a basic CAD model not only saves time in the design process but provides an excellent platform to communicate ideas. The user has the abil... (more)
Created Date 2017
Contributor Anderson, Benjamin Kyle (Author) / Takahashi, Timothy (Advisor) / Bolukbasi, Akif (Committee member) / Patel, Jay (Committee member) / Arizona State University (Publisher)
Subject Aerospace engineering / Design
Type Masters Thesis
Extent 115 pages
Language English
Copyright
Reuse Permissions All Rights Reserved
Note Masters Thesis Aerospace Engineering 2017
Collaborating Institutions Graduate College / ASU Library
Additional Formats MODS / OAI Dublin Core / RIS


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Description Dissertation/Thesis