Fatigue life methodology for tapered composite flexbeam laminates

Annual Forum Proceedings - American Helicopter Society

Volumn 3, Issue , 1997, Pages 20-32

  Murri, G B ^a   O'Brien, T K ^a   Rousseau, C Q ^a  

^a Vehicle Technology Cent   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; BENDING (DEFORMATION); COMPOSITE MATERIALS; FINITE ELEMENT METHOD; FLOW OF FLUIDS; HYDRAULICS; LAMINATED COMPOSITES; LAMINATES; LOADS (FORCES); TENSILE TESTING;

ROTOR HUB FLEXBEAM;

FATIGUE OF MATERIALS;

EID: 0030643013     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)