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Volumn 4, Issue , 1999, Pages 2935-2941
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Fatigue reliability prediction of tapered composites
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC LOADS;
COMPUTER SIMULATION;
FAILURE ANALYSIS;
FATIGUE OF MATERIALS;
FINITE ELEMENT METHOD;
HELICOPTER ROTORS;
PARAMETER ESTIMATION;
PROBABILITY;
RELIABILITY;
STRUCTURAL DESIGN;
BENDING LOADS;
CENTRIFUGAL LOAD;
FATIGUE RELIABILITY PREDICTION;
FIRST ORDER RELIABILITY ANALYSIS;
ROTOR HUBS;
TAPERED COMPOSITES;
COMPOSITE STRUCTURES;
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EID: 0032666537
PISSN: 02734508
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.1999-1586 Document Type: Article |
Times cited : (3)
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References (15)
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