Towards simulation of flapping wings using immersed boundary method

Author:

Zhang X. Q.1,Theissen P.2,Schlüter J. U.1

Affiliation:

1. School of Mechanical and Aerospace Engineering; Nanyang Technological University; 50, Nanyang Avenue; 639798; Singapore

2. Institute of Aerodynamics; Technical University of Munich; Boltzmannstr. 15; D-85748; Garching; Germany

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference31 articles.

1. Leading-edge vortex improves lift in slow-flying bats;Muijres;Science,2008

2. Flapping wings and aerodynamic lift: the role of leading-edge vortices;Shyy;American Institute of Aeronautics And Astronautics,2007

3. Peskin CS Flow patterns around heart valves: a digital computer method for solving the equations of motion PhDthesis 1972 378 72 30

4. Wall modeling for large-eddy simulation using an immersed boundary method;Tessicini;Center for Turbulence Research, Annual Research Briefs,2002

5. IMMERSED BOUNDARY METHODS

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