Aeroelastic stability of hingeless rotor blade in hover using large deflection theory

DOI10.2514/3.12217zbMath0810.73020OpenAlexW2010404186MaRDI QIDQ4317330

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Publication date: 18 April 1995

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.12217

zbMATH Keywords

Hamilton's principlestability boundary\(p-k\) modal flutter analysisflap-lag-torsioniterative Newton-Raphson methodtwo-dimensional strip theories

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) Stability of dynamical problems in solid mechanics (74H55)

Related Items (2)

Nonlinear aeroelastic stability analysis of hingeless helicopter rotor blades using FRF coupling and condition number ⋮ FLUID-STRUCTURE INTERACTION ANALYSIS OF HINGELESS ROTOR BLADES IN HOVER CONSIDERING WAKE EFFECTS

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