Pages that link to "Item:Q413122"
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The following pages link to Active control of supersonic/hypersonic aeroelastic flutter for a two-dimensional airfoil with flap (Q413122):
Displaying 11 items.
- Specially orthotropic panel flutter control using PID controller (Q1956415) (← links)
- Robust aeroelastic control of two-dimensional supersonic flapped wing systems (Q2385312) (← links)
- Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow (Q2393538) (← links)
- Advances in the linear/nonlinear control of aeroelastic structural systems (Q2575192) (← links)
- Active control of hypersonic airfoil flutter via adaptive fuzzy sliding mode method (Q2832371) (← links)
- Analytical and Experimental Aeroelastic Wing Flutter Analysis and Suppression (Q2972416) (← links)
- A comparison of full non-linear and reduced order aerodynamic models in control law design using a two-dimensional aerofoil model (Q3425341) (← links)
- ACTIVE AEROELASTIC CONTROL OF LIFTING SURFACES VIA JET REACTION LIMITER CONTROL (Q3498667) (← links)
- (Q3561504) (← links)
- Adaptive aeroelastic vibration suppression of a supersonic airfoil with flap (Q4929492) (← links)
- Vibration suppression on the composite laminated plates subjected to aerodynamic and harmonic excitations based on the nonlinear piezoelectric shunt damping (Q6072750) (← links)
