Dissertation/Thesis Abstract

A study comparing changes in loading conditions of an extended service life system using aluminum 2024-T351
by Beal, Roger Zack, M.S., The University of Utah, 2014, 324; 1569706
Abstract (Summary)

The current fiscally austere environment prevalent in the military and industry is driving extreme measures to save money. In the United States Air Force, this has driven enormous efforts to trim sustainment spending on extended life aircraft. The challenge to the aerospace engineer is to ensure flight safety in the midst of this economic pressure.

One method of cutting costs is to increase the time an aircraft is in service by delaying the point when the aircraft is taken out of service for depot maintenance. To ensure flight safety, in depth fatigue and fracture analysis needs to be accomplished to assess increasing the inspection interval.

The purpose of this study was to determine the sensitivity of Aluminum 2024-T351 alloy, a common material used in tension dominated aerospace applications, to two different loading spectra—one that is aggressive and the other that is benign. This was accomplished by conducting five different combinations of the two spectra, developing computer simulations using the AFGROW software and comparing with the measured data. The results showed that the material demonstrated significantly different behavior between the two spectra. These results provide a valuable tool for the aerospace engineer for fatigue life prediction and inspection interval evaluation.

Indexing (document details)
Advisor: Hoeppner, David W.
Commitee: Adams, Daniel O., Thomsen, Mark L.
School: The University of Utah
Department: Mechanical Engineering
School Location: United States -- Utah
Source: MAI 54/01M(E), Masters Abstracts International
Subjects: Mechanics, Aerospace engineering, Mechanical engineering
Publication Number: 1569706
ISBN: 978-1-321-36003-5
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