Aeroservoelastic design optimization with experimental verification

Journal of Aircraft

Volumn 38, Issue 5, 2001, Pages 958-961

  Borglund, D ^a  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; CONTROL SYSTEM ANALYSIS; ELASTICITY; OPTIMIZATION; WIND TUNNELS;

AEROSERVOELASTICITY;

FLIGHT DYNAMICS;

EID: 0035438722     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2860     Document Type: Article

References (11)

1. Aeroelastic tailoring of composite structures
2. Aeroelastic design optimization with experimental verification
3. Active flutter suppression for a wing model
4. Active nozzle control and integrated design optimization of a beam subject to fluid-dynamic forces
5. Active wing flutter suppression using a trailing edge flap
6. Optical measurements of flutter mode shapes
7. On the convergence of methods for nonlinear eigenvalue problems
8. The Method of Moving Asymptotes (MMA) with some extensions
9. Sensitivity of discrete systems