Flap-torsion coupling in sandwich beams and filled box sections

Thin-Walled Structures

Volumn 43, Issue 6, 2005, Pages 923-955

  Lemanski, Stuart ^a   Weaver, Paul ^a  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

Author keywords

Aeroelastic tailoring; Box beam; Composite; Sandwich

Indexed keywords

BEAMS AND GIRDERS; COMPOSITE STRUCTURES; ELASTICITY; FINITE ELEMENT METHOD; HELICOPTER ROTORS; MATHEMATICAL MODELS; SANDWICH STRUCTURES; STIFFNESS; TURBOMACHINE BLADES;

AERODYNAMIC STRUCTURES; AEROELASTIC TAILORING; BOX BEAMS;

AERODYNAMICS;

EID: 17444382691     PISSN: 02638231     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.tws.2004.12.004     Document Type: Article

References (5)

1. Smith EC. Aeroelastic response and aeromechanical stability of helicopters with elastically coupled composite rotor blades. PhD Thesis. University of Maryland; 1992.
2. L.W. Rehfield, A.R. Atilgan, and D.H. Hodges Nonclassical behaviour of thin-walled composite beams with closed cross sections J Am Helicopter Soc 35 2 1990 42 50
3. L.W. Rehfield A refined simple model for tailoring box beams with composites Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference, Seattle, WA 2001
4. G.F.J. Hill, and P.M. Weaver Analysis of arbitrary beam sections with non-homogeneous anisotropic material properties Proceedings of the ICCM13, Beijing, China 2001
5. Bartholomew P, Mercer AD. Analysis of an anisotropic beam with arbitrary cross-section. Technical report 84058. Royal Aircraft Establishment; 1984.