Calculations of the bounds on limit cycle oscillations in nonlinear aeroelastic systems based on equivalent linearization
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-014-5562-9.pdf
Reference24 articles.
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3. Cao D Q, Zhao N. Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap. Sci China Tech Sci, 2011, 54: 1943–1953
4. Coller B D, Chamara P A. Structural non-linearities and the nature of the classic flutter instability. J Sound Vib, 2004, 277: 711–739
5. Chen F Q, Zhou L Q, Chen Y S. Bifurcation and chaos of an airfoil with cubic nonlinearity in incompressible flow. Sci China Tech Sci, 2011, 54: 1954–1965
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