Effects of corrosion on the strength and integrity of adhesively bonded composite patch repairs of damaged aircraft structures
Keywords and Phrases
Composite patch repair
"This research investigates the effect of corrosion on composite patch repaired aluminum aircraft panels. The effect of different corrosive environments extended for various intervals of time on the mechanical and material properties was investigated and the effect of corrosion in the bonding characteristics of the adhesive and the patch was explored."--Abstract, leaf iv.
Mechanical and Aerospace Engineering
M.S. in Mechanical Engineering
University of Missouri--Rolla
Journal article titles appearing in thesis/dissertation
- Evaluation of effects of corrosion on the strength and integrity of composite patch repairs of damaged aircraft structures using acoustic emission
- Evaluation of changes in mechanical properties of composite patch repaired panels after accelerated corrosion testing
xi, 105 leaves
© 2004 Harinath Appani, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Composite materials -- Corrosion
Airplanes -- Maintenance and repair -- Materials
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=b5282122~S5
Appani, Harinath, "Effects of corrosion on the strength and integrity of adhesively bonded composite patch repairs of damaged aircraft structures" (2004). Masters Theses. 2633.