Investigation of non-linear flutter by a coupled aerodynamics and structural dynamics method-Reference-Cited by-同舟云学术

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Investigation of non-linear flutter by a coupled aerodynamics and structural dynamics method

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Sadeghi Mani¹,Liu Feng¹

Affiliation:

1. California, Univ., Irvine

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-573

Reference12 articles.

1. Computational prediction of stall flutter in cascaded airfoils

2. Computational Study of Stall Flutter in Linear Cascades

3. Time domain flutter analysis of cascades using a full-potential solver

4. proach," Journal of Propulsion and Power, Vol.15, 1999, pp.54-63.

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1. Two Better Loosely Coupled Solution Algorithms of CFD Based Aeroelastic Simulation;Engineering Applications of Computational Fluid Mechanics;2007-01

2. Reduced-order fluid/structure modeling of a complete aircraft configuration;Computer Methods in Applied Mechanics and Engineering;2006-08

3. Adaptation of POD-based Aeroelastic ROMs for Varying Mach Number and Angle of Attack: Application to a Complete F-16 Configuration;2005 U.S. Air Force T&E Days;2005-06-18

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