Efficient Method for Limit Cycle Flutter Analysis Based on Nonlinear Aerodynamic Reduced-Order Models

Authors

Keywords

Journal

Volume 50, Issue 5, Pages 1019-1028

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Online

2012-04-18

DOI

10.2514/1.j050581

References

View 6 related references

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