Masters Theses
Bonded composite patch design for aircraft structures exhibiting cracking and corrosion
Abstract
"This thesis presents the results of a study whose objective [is] to extend the applicability of the CRAS [Composite Repair of Aircraft Structures] program to include bonded patch design for aircraft structures that have sustained adjacent cracking and corrosion damage."--Abstract, page iii.
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Mechanical and Aerospace Engineering
Publisher
University of Missouri--Rolla
Publication Date
Summer 2002
Pagination
x, 78 pages
Rights
© 2002 Madhukar Singh, All rights reserved.
Document Type
Thesis - Citation
File Type
text
Language
English
Subject Headings
Airplanes -- Maintenance and repair -- MaterialsComposite materials -- Bonding
Thesis Number
T 8159
Print OCLC #
52642866
Recommended Citation
Singh, Madhukar, "Bonded composite patch design for aircraft structures exhibiting cracking and corrosion" (2002). Masters Theses. 2254.
https://scholarsmine.mst.edu/masters_theses/2254
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