Statistical fatigue of composite laminates subject to service loading spectrum

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 2148-2158

  Fu, Kwo En ^a   Lee, L J ^a   Yang, J N ^b  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

^b University of California at Irvine   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; AIRFRAMES; FATIGUE OF MATERIALS; LAMINATED COMPOSITES; LAMINATES; PHOTODEGRADATION; SOFTWARE TESTING; STIFFNESS; STRUCTURAL DYNAMICS; DEGRADATION; FAILURE (MECHANICAL); FATIGUE TESTING; LOADS (FORCES); MATERIALS TESTING; SERVICE LIFE; STATISTICAL METHODS; STRENGTH OF MATERIALS;

AIRCRAFT STRUCTURE; COMPOSITE LAMINATE; FATIGUE OF COMPOSITES; PRELIMINARY DESIGN; RESIDUAL STIFFNESS; STATISTICAL BEHAVIOR; STATISTICAL DISTRIBUTION; STIFFNESS DEGRADATION;

FIGHTER AIRCRAFT; AIRCRAFT;

FAILURE STIFFNESS; RESIDUAL STIFFNESS; SERVICE LOADING SPECTRUM; STATISTICAL DISTRIBUTIONS; STIFFNESS DEGRADATION MODEL;

EID: 0029699723     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1561     Document Type: Conference Paper

References (21)

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