A study on the robustness of two stiffened composite fuselage panels

Composite Structures

Volumn 92, Issue 2, 2010, Pages 223-232

  Lee, Merrill C W ^a   Kelly, Donald W ^a   Degenhardt, Richard ^b   Thomson, Rodney S ^c  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c Cooperative Research Centre for Advanced Composite Structures Ltd ^*  (Australia)

Author keywords

B. Defects; C. Statistical properties methods; D. Mechanical testing; Robust Design

Indexed keywords

ACCURATE PREDICTION; B. DEFECTS; C. STATISTICAL PROPERTIES/METHODS; D. MECHANICAL TESTING; EUROPEAN COMMISSION PROJECTS; INPUT VARIABLES; MANUFACTURING DEFECTS; MATERIAL VARIATION; RESEARCH PROGRAMS; ROBUST DESIGN; STIFFENED COMPOSITE; STIFFENED COMPOSITE PANEL;

DEFECTS; DESIGN; FUSELAGES; LAMINATED COMPOSITES; MECHANICAL ENGINEERING; MECHANICAL PROPERTIES; STRUCTURE (COMPOSITION);

MECHANICAL TESTING;

COMPOSITE; COMPRESSION; DEFECT; DESIGN; PREDICTION; STATISTICAL ANALYSIS; STIFFNESS; STRENGTH; STRUCTURAL ANALYSIS; TESTING;

EID: 70349795523     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2009.07.009     Document Type: Article

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