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

Document Type

Thesis - Citation

File Type

text

Language

English

Subject Headings

Airplanes -- Maintenance and repair -- Materials
Composite materials -- Bonding

Thesis Number

T 8159

Print OCLC #

52642866

Link to Catalog Record

Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.

http://merlin.lib.umsystem.edu/record=b4972506~S5

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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