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Title: Flutter speed estimation using presented differential quadrature method formulation
Authors: Ghalandari, M
Shamshirband, S
Mosavi, A
Chau, KW 
Keywords: Aero-elasticity
Subsonic regime
Deferential quadrature method (DQM)
Typical section beam
Wing design
Computational fluid dynamics (CFD)
Flutter speed prediction
Issue Date: 2019
Publisher: Taylor & Francis
Source: Engineering applications of computational fluid mechanics, 1 Jan. 2019, v. 13, no. 1, p. 804-810 How to cite?
Journal: Engineering applications of computational fluid mechanics 
Abstract: 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 speed of the structure. Based on the presented model, a code is developed, for an arbitrary typical section beam. The obtained results validated the existing methods in the literature. The proposed method provides the advantage of finding the modes of oscillation and other dynamic parameters with less than 0.2% difference.
ISSN: 1994-2060
EISSN: 1997-003X
DOI: 10.1080/19942060.2019.1627676
Rights: © 2019 The Author(s). Published by Informa UK Limited, trading as Taylor & Francis Group
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
The following publication Mohammad Ghalandari, Shahaboddin Shamshirband, Amir Mosavi & Kwokwing Chau (2019) Flutter speed estimation using presented differential quadrature method formulation, Engineering Applications of Computational Fluid Mechanics, 13:1, 804-810 is available at
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