Design, analysis and fatigue testing of adhesively bonded thick composite patch repair of aging aircraft structures
"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.
Okafor, A. Chukwujekwu (Anthony Chukwujekwu)
Mechanical and Aerospace Engineering
M.S. in Mechanical Engineering
University of Missouri--Rolla. Intelligent Systems Center
United States. Department of the Air Force
University of Missouri--Rolla
Journal article titles appearing in thesis/dissertation
- 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
xiii, 118 leaves
© 2006 Hari Bhogapurapu, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Airplanes -- Maintenance and repair -- Materials
Aluminum alloys -- Cracking
Aluminum alloys -- Fatigue
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=b5791942~S5
Bhogapurapu, Hari, "Design, analysis and fatigue testing of adhesively bonded thick composite patch repair of aging aircraft structures" (2006). Masters Theses. 5924.