Parametric aeroelastic modeling based on component modal synthesis and stability analysis for horizontally folding wing with hinge joints

DOI10.1007/S11071-017-3956-5zbMath1398.74170OpenAlexW2792611601WikidataQ130176062 ScholiaQ130176062MaRDI QIDQ1798151

Shengli Lv, Yingge Ni, Wei Zhang

Publication date: 23 October 2018

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-017-3956-5

zbMATH Keywords

flutterGram matrixaeroelasticdoublet lattice methodcomponent modal synthesisfolding wing

Mathematics Subject Classification ID

Stability of dynamical problems in solid mechanics (74H55)

Related Items (1)

Subcritical and supercritical nonlinear aeroelastic behavior of a morphing wing with bilinear hinge stiffness

Cites Work

• Principal component analysis in linear systems: Controllability, observability, and model reduction
• Actuator and Exciter Placement for Flexible Structures
• MODEL REDUCTION FOR FLUIDS, USING BALANCED PROPER ORTHOGONAL DECOMPOSITION

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