Residual tension strength study of fatigued open-hole titanium-graphite hybrid composite laminates

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 1998, Pages 2098-2105

  Li, Edward ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; CRACK PROPAGATION; FATIGUE TESTING; GRAPHITE; NONMETALLIC MATRIX COMPOSITES; RESIDUAL STRESSES; TENSILE STRENGTH; TITANIUM;

DAMAGE TOLERANCE; HYBRID COMPOSITE LAMINATES; POLYMER MATRIX COMPOSITES; RESIDUAL STRENGTH;

LAMINATED COMPOSITES;

EID: 0031700393     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1960     Document Type: Conference Paper

References (3)