Experiments and analyses on post-buckling behavior of stringer-stiffened laminated composite helicopter tailplane

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

Volumn 2, Issue , 2005, Pages 759-773

  Bisagni, Chiara ^a,b   Giavotto, Vittorio ^a,b  

^a POLITECNICO DI MILANO   (Italy)

^b Department of Aerospace Engineering ^*  (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; CARBON; COMPRESSION TESTING; CORRELATION METHODS; EMPENNAGES; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; STIFFNESS; STRUCTURAL PANELS;

CARBON FABRICS; LOAD CELL; POST-BUCKLING; TARGET LOAD;

HELICOPTERS;

EID: 28844492627     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1866     Document Type: Conference Paper

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