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Optimizing induced strain actuators for maximum panel deflection

T. Leeks | Terrence Wesshaar | Tamara Leeks | Terrence Wesshaar

[1] P. Hajela,et al. Application of piezoelectric elements in supersonic panel flutter suppression , 1991 .

[2] On Large Deflection Effects in Unsymmetric Cross-Ply Composite Laminates , 1988 .

[3] George S. Dulikravich,et al. Transonic airfoil thickness variation requirements for maintaining shock-free flow , 1993, Smart Structures.

[4] Craig A. Rogers,et al. Laminate Plate Theory for Spatially Distributed Induced Strain Actuators , 1991 .

[5] S. J. Kim,et al. Optimal design of piezoactuators for active noise and vibration control , 1991 .

[6] T. A. Weisshaar,et al. Controlling panel flutter using adaptive materials , 1991 .

[7] Kenneth B. Lazarus,et al. Induced strain actuation of isotropic and anisotropic plates , 1991 .

[8] Robert C. Scott,et al. Active control of composite panel flutter using piezoelectric materials , 1993, Smart Structures.

[9] C. W. Bert,et al. Mechanics of composite structures , 1993 .

[10] J. Jia,et al. BEHAVIOR OF SHAPE MEMORY ALLOY REINFORCED COMPOSITE PLATES PART I: Model Formulations and Control Concepts , 1989 .

[11] C. Sun,et al. Analysis of asymmetric composite laminates , 1988 .