{"title":"Closed-loop subsonic flutter control of smart symmetric variable stiffness composite laminates in tapered-swept configurations","authors":"Pritam Mondal, Prashanta Kr. Mahato","doi":"10.1016/j.euromechsol.2025.105875","DOIUrl":null,"url":null,"abstract":"<div><div>This study investigates the free vibration, transient dynamic response, and flutter characteristics of cantilevered smart symmetric variable-stiffness composite laminated (VSCL) plates, focusing on both forward-swept and backward-swept tapered configurations with identical aspect ratios. Closed-loop vibration control using active fibre composites (AFCs) as actuators and sensors is implemented, incorporating a full-state feedback controller. Additionally, the effect of the plate's geometry on the flutter characteristics of VSCL plates is examined. A MATLAB-based finite element (FE) code is employed for normal mode analysis. A simple and effective methodology is used for meshing swept tapered plates. Unsteady aerodynamic forces are calculated using the doublet lattice method (DLM) in MSC Nastran for flutter analysis under subsonic flow conditions. The aerodynamic model is integrated with structural modal parameters via direct matrix abstraction programming (DMAP) in Nastran. Results show that forward-swept plates are prone to divergence, while backward-swept plates exhibit controlled flutter behaviour with the implemented controller.</div></div>","PeriodicalId":50483,"journal":{"name":"European Journal of Mechanics A-Solids","volume":"116 ","pages":"Article 105875"},"PeriodicalIF":4.2000,"publicationDate":"2025-09-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"European Journal of Mechanics A-Solids","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0997753825003092","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0
Abstract
This study investigates the free vibration, transient dynamic response, and flutter characteristics of cantilevered smart symmetric variable-stiffness composite laminated (VSCL) plates, focusing on both forward-swept and backward-swept tapered configurations with identical aspect ratios. Closed-loop vibration control using active fibre composites (AFCs) as actuators and sensors is implemented, incorporating a full-state feedback controller. Additionally, the effect of the plate's geometry on the flutter characteristics of VSCL plates is examined. A MATLAB-based finite element (FE) code is employed for normal mode analysis. A simple and effective methodology is used for meshing swept tapered plates. Unsteady aerodynamic forces are calculated using the doublet lattice method (DLM) in MSC Nastran for flutter analysis under subsonic flow conditions. The aerodynamic model is integrated with structural modal parameters via direct matrix abstraction programming (DMAP) in Nastran. Results show that forward-swept plates are prone to divergence, while backward-swept plates exhibit controlled flutter behaviour with the implemented controller.
期刊介绍:
The European Journal of Mechanics endash; A/Solids continues to publish articles in English in all areas of Solid Mechanics from the physical and mathematical basis to materials engineering, technological applications and methods of modern computational mechanics, both pure and applied research.