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Volumn , Issue , 1996, Pages 322-330
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Failure mechanisms around the interface between a sandwich skin and a bonded frame
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Author keywords
[No Author keywords available]
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Indexed keywords
AIRCRAFT MANUFACTURE;
AIRFRAMES;
STRUCTURAL DYNAMICS;
ADHESIVES;
FAILURE (MECHANICAL);
FINITE ELEMENT METHOD;
FORECASTING;
INTERFACES (MATERIALS);
LOADS (FORCES);
MATHEMATICAL MODELS;
MECHANICAL TESTING;
SANDWICH STRUCTURES;
STRENGTH OF MATERIALS;
STRESS ANALYSIS;
STRUCTURAL FRAMES;
ADVANCED TECHNOLOGY;
COMPOSITE AIRCRAFT STRUCTURE;
FAILURE MECHANISM;
FAILURE PREDICTION;
INTERLAMINAR FAILURES;
INTERLAMINAR STRESS;
INTERLAMINAR TENSION;
TEST CONFIGURATIONS;
FINITE ELEMENT METHOD;
BOND STRENGTH (MATERIALS);
BONDED FRAME;
CORE TRANSVERSE SHEAR FAILURE;
FAILURE LOAD;
FINITE ELEMENT MODELS;
INTERLAMINAR FAILURE;
INTERLAMINAR STRESSES;
PULL OFF STRENGTH TEST;
PUSH IN STRENGTH TEST;
SANDWICH SKIN;
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EID: 0029706509
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.1996-1353 Document Type: Conference Paper |
Times cited : (1)
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References (6)
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