Aeroelastic response of a coupled rotor/fuselage system in hovering and forward flight

DOI10.1007/S004190050205zbMath0949.74019OpenAlexW2009250549MaRDI QIDQ1307740

V. Pereyra

Publication date: 8 February 2000

Published in: Archive of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s004190050205

zbMATH Keywords

Hamilton's principlehelicopter dynamicsiterative solutionblade aeroelastic responsecoupled rotor/fuselage systemfive-node 15-DOF pre-twisted nonuniform beam elementmoderate-deflection beam theorymodified quasi-linearization methodresponse of fuselagetwo-dimensional quasi-steady aerodynamic model

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05)

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