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Showing 1 to 1 of 1 for “"Non-uniform Beam Finite Element"”.

  1. Effect of Compressive Force on Aeroelastic Stability of a Strut-Braced Wing

    … stability of the SBW using efficient structural finite element and aerodynamic lifting surface methods. A procedure is developed to generate wing stiffness distribution for detailed and simplified wing models and to include the compressive force effect in the SBW aeroelastic analysis. A …

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