Parametric aeroelastic modeling based on component modal synthesis and stability analysis for horizontally folding wing with hinge joints
type: Item
instance of: scholarly article
title: Parametric aeroelastic modeling based on component modal synthesis and stability analysis for horizontally folding wing with hinge joints
zbMATH Open document ID: 1398.74170
author: Wei Zhang
author: Shengli Lv
author: Yingge Ni
published in: Nonlinear Dynamics
publication date: 2018-10-23T00:00:00Z
Mathematics Subject Classification ID: 74H55
zbMATH DE Number: 6962359
zbMATH Keywords: folding wing
zbMATH Keywords: component modal synthesis
zbMATH Keywords: doublet lattice method
zbMATH Keywords: aeroelastic
zbMATH Keywords: flutter
zbMATH Keywords: Gram matrix
MaRDI profile type: Publication
full work available at URL: s11071-017-3956-5
OpenAlex ID: W2792611601
cites work: Principal component analysis in linear systems: Controllability, observability, and model reduction
cites work: Actuator and Exciter Placement for Flexible Structures
cites work: MODEL REDUCTION FOR FLUIDS, USING BALANCED PROPER ORTHOGONAL DECOMPOSITION
Wikidata QID: Q130176062
DOI: 10.1007/S11071-017-3956-5
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description: scientific article; zbMATH DE number 6962359