Finite element analysis of the geometric stiffening effect. Part 2: Non-linear elasticity

Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-body Dynamics

Volumn 219, Issue 2, 2005, Pages 203-211

  Garcia Vallejo D ^a   Sugiyama, H ^b   Shabana, A A ^b  

^a UNIVERSITY OF SEVILLE   (Spain)

^b University of Illinois at Chicago   (United States)

Author keywords

Absolute nodal coordinate formulation; Geometric stiffening; Helicopter blade; Non linear elasticity; Rotating beams; Stability

Indexed keywords

ELASTICITY; EQUATIONS OF MOTION; HELICOPTERS; NONLINEAR SYSTEMS; STIFFNESS; TURBOMACHINE BLADES;

ABSOLUTE NODAL COORDINATE FORMULATION; GEOMETRIC STIFFENING; HELICOPTER BLADES; NON-LINEAR ELASTICITY;

FINITE ELEMENT METHOD;

EID: 23444437655     PISSN: 14644193     EISSN: None     Source Type: Journal    
DOI: 10.1243/146441905X10050     Document Type: Conference Paper

References (14)

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