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Theses/Dissertations
Author Bhogapurapu, Hari, 1981-

Title Design, analysis and fatigue testing of adhesively bonded thick composite patch repair of aging aircraft structures / by Hari Bhogapurapu.

Published ©2006.
LOCATION CALL # STATUS
 MST DEPOSITORY  THESIS T 9021/9045  MICROFILM    NOT CHECKED OUT
 MST Thesis  THESIS T 9031    NOT CHECKED OUT
Description xiii, 118 leaves : illustrations ; 28 cm.
Summary "This thesis presents the results of the research on the design, fabrication, analysis and fatigue testing of adhesively bonded thick composite patch repair of circular corrosion grind-out and crack propagating on the periphery of the corrosion grind-out on 2024 T3 Clad aluminum aircraft panel"--Abstract, leaf iv.
Notes Vita.
Includes bibliographical references.
M.S. University of Missouri--Rolla 2006.
Subjects Airplanes -- Maintenance and repair -- Materials.
Composite materials -- Bonding.
Aluminum alloys -- Fatigue.
Aluminum alloys -- Cracking.
Other Titles MST thesis. Mechanical Engineering (M.S., 2006).
Design and analysis of adhesively bonded thick composite patch repair of corrosion grind-out and cracks on 2024 T3 clad aluminum aging aircraft structures.
Design and analysis of adhesively bonded thick elliptical composite patch repair and comparison with octagonal patch repair of aging aircraft structures.
Fatigue crack propagation and finite element analysis of perfectly and imperfectly bonded thick elliptical and octagonal composite patch repair of aluminum aircraft structures.
OCLC/WorldCat Number 85766749
Permanent Link
http://merlin.lib.umsystem.edu:80/record=b5791942~S5