Abstract In the present contribution concepts of reduced structural models for Computational Aero-Elastic simulation (CAE) on aircraft wings are presented. Here the idealization approach relies on analytical methods with the aim to shorten in comparison to a typical finite element method computational cost and time, by preserving nearly the same accuracy. Prior to more detailed investigations using higher order models, these simplified models allow an earlier access of insight regarding the aeroelastic and structural behavior of the wing at the very beginning of the design process. At first a one-dimensional idealization that extends the Timoshenko beam by taking into account additional effects due to warpings is developed. To better describe the influence of swept, a three dimensional idealization is derived. Both idealizations yield good agreements in results concerning the global static deformation and the modal behavior of the wing.
Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity
01.01.2010
25 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Timoshenko Beam , Structural Idealization , Spanwise Direction , Aircraft Wing , Normal Stress Distribution Engineering , Aerospace Technology and Astronautics , Classical Continuum Physics , Engineering Fluid Dynamics , Appl.Mathematics/Computational Methods of Engineering , Fluid- and Aerodynamics , Numerical and Computational Physics
Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity
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