Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap

DOI10.1007/s11431-011-4467-0zbMath1237.76064OpenAlexW1967728259MaRDI QIDQ413122

Na Zhao, Dengqing Cao

Publication date: 4 May 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4467-0

zbMATH Keywords

active controlnonlinearity2-D airfoilflutter/post fluttersupersonic/hypersonic flow

Mathematics Subject Classification ID

Adaptive control/observation systems (93C40) Supersonic flows (76J20) Hypersonic flows (76K05)

Related Items (2)

Vibration suppression on the composite laminated plates subjected to aerodynamic and harmonic excitations based on the nonlinear piezoelectric shunt damping ⋮ Analytical and Experimental Aeroelastic Wing Flutter Analysis and Suppression

Cites Work

• Unnamed Item
• Unnamed Item
• Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
• The flutter of an airfoil with cubic structural and aerodynamic non-linearities

This page was built for publication: Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap