Geometrically nonlinear aeroelastic behavior of pretwisted composite wings modeled as thin walled beams

Author:

Farsadi Touraj,Rahmanian Mohammad,Kayran Altan

Funder

RÜZGEM-Center for Wind Energy Research in METU

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference49 articles.

1. Study of effects of sweep on the flutter of cantilever wings;Barmby,1951

2. A geometrically non-linear theory for laminated anisotropic thin-walled beams;Bhaskar;Internat. J. Engrg. Sci.,1995

3. Aeroelasticity;Bisplinghoff,2013

4. Analysis and Design of Flight Vehicle Structures;Bruhn,1973

5. Carlo. Cesnik, D.H., Patil, M., Aeroelastic analysis of composite wings. In: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference and Exhibit, 37th, 15–17 April 1996, Salt Lake City, UT, USA, pp. 1113–1123.

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