Flutter speed estimation using presented differential quadrature method formulation

Flutter speed estimation using presented differential quadrature method formulation

In this paper the flutter behavior of a typical wing is investigated. The study is performed by presented Deferential Quadrature Method (DQM). The aerodynamic part adopted Wagner functions to model subsonic regime. Quasi steady and unsteady aerodynamics are considered to estimate the instability spe...

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Bibliographic Details
Main Authors: Mohammad Ghalandari, Shahaboddin Shamshirband, Amir Mosavi, Kwok-wing Chau
Format: Article
Language:English
Published: Taylor & Francis Group 2019-01-01
Series:Engineering Applications of Computational Fluid Mechanics
Subjects:
aero-elasticity
subsonic regime
deferential quadrature method (dqm)
typical section beam
aerodynamic
wing design
airfoil
computational fluid dynamics (cfd)
flutter speed prediction
Online Access:http://dx.doi.org/10.1080/19942060.2019.1627676

Internet

http://dx.doi.org/10.1080/19942060.2019.1627676

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