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Experimental modal analysis of a rotor with active composite blades

https://doi.org/10.1016/j.compstruct.2016.06.013

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

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Free vibration of generally layered composite beams using symbolic computations

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Integration of active vibration control methods with finite element models of smart laminated composite structures

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Dynamic finite element method for generally laminated composite beams

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Dynamics of a composite Timoshenko beam with delamination

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Active vibration control based on piezoelectric smart composite

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Experimental identification of smart material coupling effects in composite structures

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Modelling and Simulation of 3 Blade Helicopter's Rotor Model

inferredcites →https://doi.org/10.15660/auofmte.2014-1.2964openalex-snapshot

STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE

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Modular Analysis of Main Rotor Blade of Light Helicopter using FEM

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Application of 3-D Laser Scanning Vibrometer in Determination of Free Vibration Frequencies of Composite Plates with Damage

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Active Vibration Control of Piezoelectric Intelligent Structures

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Finite Element Modeling of a Piezoelectric Composite Beam and Comparative Performance Study of Piezoelectric Materials for Voltage Generation

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