Nondestructive evaluation of corrosion in aging aircraft structures and its effect on structural integrity
"This research can be divided into two subtopics. The first subtopic presents the results of multifrequency eddy current inspection of corrosion damage and machined material loss in clad aluminum 2024-T3 riveted lap joint specimens and its effect on the fatigue life...The second subtopic investigates the effect of strain-rate and corrosion on material properties and acoustic emission (AE) of clad aluminum 2024-T3 during tension testing"--Abstract, leaf iv.
Okafor, A. Chukwujekwu (Anthony Chukwujekwu)
Dharani, Lokeswarappa R.
Mechanical and Aerospace Engineering
M.S. in Manufacturing Engineering
Society of Manufacturing Engineers. Education Foundation
United States. Department of the Air Force
University of Missouri--Rolla
Journal article titles appearing in thesis/dissertation
- Multifrequency eddy current inspection of corrosion in clad aluminum riveted lap joints and its effect on fatigue life
- Effect of strain-rate and corrosion on material properties and acoustic emissions in clad aluminum 2024-T3 during tension testing
xii, 99 leaves
© 2006 Shridhar Natarajan, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Accelerated life testing
Acoustic emission testing
Airframes -- Fatigue -- Testing
Corrosion and anti-corrosives -- Testing
Eddy currents (Electric)
Print OCLC #
Link to Catalog Record
Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.http://laurel.lso.missouri.edu/record=b5795620~S5
Natarajan, Shridhar, "Nondestructive evaluation of corrosion in aging aircraft structures and its effect on structural integrity" (2006). Masters Theses. 3975.