Fatigue damage in titanium-graphite hybrid laminates

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

Volumn 3, Issue , 1998, Pages 2088-2097

  Burianek, Dennis A ^a   Spearing, S Mark ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; COMPRESSIVE STRENGTH; CRACK INITIATION; DELAMINATION; FATIGUE TESTING; GRAPHITE; HIGH TEMPERATURE EFFECTS; STIFFNESS; TENSILE STRENGTH; TITANIUM;

DAMAGE PROGRESSION; FACESHEET DELAMINATION; HYBRID LAMINATES; STIFFNESS MEASUREMENTS;

LAMINATED COMPOSITES;

EID: 0031704781     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)