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Volumn 41, Issue 1, 1996, Pages 532-543
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Effectiveness of an adhesively bonded composite patch repair as applied to a transport aircraft lower wing skin
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Author keywords
[No Author keywords available]
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Indexed keywords
ADHESIVES;
AIRCRAFT MATERIALS;
AIRCRAFT PARTS AND EQUIPMENT;
BONDING;
CRACK PROPAGATION;
FATIGUE TESTING;
INSPECTION;
REPAIR;
TRANSPORT AIRCRAFT;
ULTRASONIC APPLICATIONS;
WINGS;
COMPOSITE PATCH REPAIR;
FATIGUE CRACK GROWTH;
LOWER WING SKIN;
SIMULATED FLIGHT LOADING;
COMPOSITE STRUCTURES;
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EID: 0029699655
PISSN: 08910138
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Article |
Times cited : (7)
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References (3)
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