Transonic flutter analysis of an AGARD 445.6 wing in the frequency domain using the Euler method-Reference-Cited by-同舟云学术

Transonic flutter analysis of an AGARD 445.6 wing in the frequency domain using the Euler method

Published:2016-01 Issue:1 Volume:10 Page:243-254
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Zhang Bocheng,Ding Weilong,Ji Shengcheng,Zhang Jiazhen

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2016.1152200

Reference21 articles.

1. Errata: "Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows"

2. Fluid Structure Interaction of Unsteady Aerodynamics of Flapping Wing at Low Reynolds Number

3. Foerster, M. & Breitsamter C. (2013, June).Computational aeroelastic analysis in time and frequency domain using non-linear and linearized Euler/Navier-Stokes methods. Paper presented at the meeting of International Forum on Aeroelasticity & Structural Dynamics, Bristol, UK.

4. Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary Conditions

5. Numerical Simulation of Limit-cycle Oscillations of a Cropped Delta Wing Using the Full Navier-Stokes Equations

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