Bonded composite patch design for aircraft structures exhibiting cracking and corrosion
"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.
Mechanical and Aerospace Engineering
M.S. in Mechanical and Aerospace Engineering
University of Missouri--Rolla
x, 78 pages
© 2002 Madhukar Singh, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Airplanes -- Maintenance and repair -- Materials
Composite materials -- Bonding
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=b4972506~S5
Singh, Madhukar, "Bonded composite patch design for aircraft structures exhibiting cracking and corrosion" (2002). Masters Theses. 2254.
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