An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps

DOI10.1016/j.ast.2003.10.003zbMath1062.74588OpenAlexW2083098599MaRDI QIDQ4651821

Sathyamangalam Ramanarayanan Viswamurthy, Ranjan Ganguly

Publication date: 22 February 2005

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ast.2003.10.003

zbMATH Keywords

OptimizationVibrationAeroelasticityHelicopterTrailing edge flaps

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05) Optimization of other properties in solid mechanics (74P10)

Related Items (3)

Performance sensitivity of helicopter global and local optimal harmonic vibration controller ⋮ Fractal boundaries of basin of attraction of Newton-Raphson method in helicopter trim ⋮ Using the Complete Authority of Multiple Active Trailing-edge Flaps for Helicopter Vibration Control

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