Fully Coupled Aeroelastic Analyses of Wing Flutter towards Application to Complex Aircraft Configurations

Author:

Yuan Weixing1,Sandhu Rimple2,Poirel Dominique3

Affiliation:

1. Senior Research Officer, Aerospace Research Centre, National Research Council Canada, Ottawa, ON, Canada K1A 0R6 (corresponding author).

2. Ph.D. Student and Visiting Scholar at the National Research Council Canada, Dept. of Civil and Environmental Engineering, Carleton Univ., Ottawa, ON, Canada K1S 5B6; presently, Postdoctoral Researcher, National Wind Technology Center, National Renewable Energy Laboratory, 15013 Denver W Pkwy., Golden, CO 80401.

3. Professor, Dept. of Mechanical and Aerospace Engineering, Royal Military College of Canada, Kingston, ON, Canada K7K 7B4.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference43 articles.

1. Beaubien R. J. F. Nitzsche and D. Feszty. 2005. “Time and frequency domain solutions for the AGARD 445.6 wing.” In Proc. Int. Forum on Aeroelasticity and Structural Dynamics. Bonn Germany: German Aerospace Society.

2. Review of unsteady transonic aerodynamics: Theory and applications

3. Bohbot J. and D. Darracq. 2001. “Time domain analysis of two D.O.F. airfoil flutter using an Euler/turbulent Navier–Stokes implicit solver.” In Proc. Int. Forum on Aeroelasticity and Structural Dynamics. Madrid Spain: Confederation of European Aerospace Societies.

4. Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings

5. Brown S. A. 1997. “Displacement extrapolation for CFD-CSM aeroelastic analysis.” In Proc. 38th Structures Structural Dynamics and Materials Conf. Reston VA: American Institute of Aeronautics and Astronautics.

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