论文信息 - Static aeroelastic control of an adaptive lifting surface

Static aeroelastic control of an adaptive lifting surface

Piezoelectric actuators are embedded in an idealized laminated composite wing structure that can adapt to changing flight conditions. A feedback control system senses wing roots strains and then applies a proportional voltage to active actuator layers to change wing lift or divergence dynamic pressure

T. A. Weisshaar | S. M. Ehlers | S. Ehlers | Terrence A. Weisshaar

[1] C. M. Wayman,et al. The Shape Memory (‘Marmem’) Effect in Alloys , 1972 .

[2] Martin Goland,et al. Principles of aeroelasticity , 1975 .

[3] E. Crawley,et al. Static Aeroelastic Control Using Strain Actuated Adaptive Structures , 1991 .

[4] George Anastas,et al. Distributed Magnetic Actuators for Fine Shape Control , 1988 .

[5] Raphael T. Haftka,et al. An analytical investigation of shape control of large space structures by applied temperatures , 1985 .

[6] Kenji Uchino,et al. New Electromechanical Materials and Their Applications , 1981 .

[7] Richard O. Claus,et al. Optical fiber sensors and signal processing for smart materials and structures applications , 1989 .

[8] E. Crawley,et al. Use of piezoelectric actuators as elements of intelligent structures , 1987 .

[9] T. Weisshaar. Aeroelastic Tailoring of Forward Swept Composite Wings , 1981 .

[10] R. M. Measures,et al. Smart structures with nerves of glass , 1989 .

[11] Donald L. Edberg. Control of flexible structures by applied thermal gradients , 1987 .

[12] E G Wilson. Static Aeroelasticity in the Design of Modern Fighters , 1986 .