Active wing flutter suppression using a trailing edge flap

Journal of Fluids and Structures

Volumn 16, Issue 3, 2002, Pages 271-294

  Borglund, D ^a   Kuttenkeuler, J ^a  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; FLUTTER; WING;

EID: 0035997576     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.2001.0426     Document Type: Article

References (28)

1. On the convergence of methods for nonlinear eigenvalue problems
2. Active flutter control using generalized unsteady aerodynamic theory
3. Active flutter suppression for a wing model
4. Sensitivity of discrete systems
5. Design for active flutter suppression and gust alleviation using state-space modeling
6. Optical measurements of flutter mode shapes
7. A finite element based modal method for determination of plate stiffnesses considering uncertainties
8. Aeroelastic design optimization with experimental verification
9. Aeroelastic tailoring considering uncertainties in material properties
10. Numerical simulations of flutter and its suppression by active control
11. Benchmark active control technology special section, Part I
12. Benchmark active control technology special section, Part II
13. Benchmark active control technology special section, Part III
14. Eigenvalues in optimum structural design
15. The method of moving asymptotes (MMA) with some extensions
16. Experimental active control of a typical section using a trailing-edge flap
17. Active flutter suppression for the active flexible wing
18. Parameter estimation and analysis of actuators for the BACT wind-tunnel model
19. Vibration tailoring of advanced composite lifting surfaces