References
- Dowell, E. H., Clark, R., Cox, D., Curtiss, H. C. JR., Edwards, J. W., Hall, K. C., Peters, D. A., Scanlan, R., Simiu, E., Sisto, F. and Strganac, T. W., 2004, A Modern Course in Aeroelasticity, 4th edition, Kluwer Academic Publishers, New York.
- Hodges, D. H. and Pierce, G. A., 2002, Introduction to Structural Dynamics and Aeroelasticity, Cambridge University Press, Cambridge.
- Garrick, I. E. and Reed, W. H. III, 1981, Historical Development of Aircraft Flutter, Journal of Aircraft, Vol. 18, No. 11, pp. 897-912. https://doi.org/10.2514/3.57579
- Bennett, R. M., Batina, J. T. and Cunningham, H. J., 1989, Wing-flutter Calculations with the CAP-TSD Unsteady Transonic Small-disturbance Program, Journal of Aircraft, Vol. 26, No. 9, pp. 876-882. https://doi.org/10.2514/3.45854
- Shin, W. H., Bae, J. S., Lee, I., Han, J. H., Shin, Y. S. and Lee, Y. W., 2005, Nonlinear Flutter Analysis of Missile Fin Considering Dynamic Stiffness of Actuator, Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 33, No. 2, pp. 54-59. https://doi.org/10.5139/JKSAS.2005.33.2.054
- Kim, D. H., Oh, S. W. and Lee, J. J., 2006, Virtual Flutter Test of a Spanwise Curved Wing Using CFD/CSD Integrated Coupling Method, Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 16, No. 4, pp. 355-365. https://doi.org/10.5050/KSNVN.2006.16.4.355
- Kim, D. H., Kim, Y. S., Kim, Y. H. and Oh, I. K., 2008, Supersonic and Hypersonic Flutter Characteristics for Various Typical Section Shapes of Missile Fin, Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 18, No. 5, pp. 496-502. https://doi.org/10.5050/KSNVN.2008.18.5.496
- Mason, G. S. and Berg, M. C., 1994, Multirate Flutter Suppression System Design for a Model Wing, Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, pp. 1267-1274. https://doi.org/10.2514/3.21343
- Eversman, W. and Roy, I. D., 1997, Active Flutter Suppression Using Multi-input/multi-output Adaptive Least Mean Square Control, Journal of Aircraft, Vol. 34. No.2, pp. 244-250. https://doi.org/10.2514/2.2163
- Vipperman, J. S., Clark, R. L., Conner, M. and Dowell, E. H., 1998, Experimental Active Control of a Typical Section Using a Trailing-edge Flap, Journal of Aircraft, Vol. 35, No. 2, pp. 224-229. https://doi.org/10.2514/2.2312
- Han, J. H., Tani, J. and Qiu, J., 2006, Active Flutter Suppression of a Lifting Surface Using Piezoelectric Actuation and Modern Control Theory, Journal of Sound and Vibration, Vol. 291, No. 3-5, pp. 706-722. https://doi.org/10.1016/j.jsv.2005.06.029
- Kim, D.-H., Han, J. H. and Lee, I., 2004, Application of Fiber Optic Sensor and Piezoelectric Actuator to Flutter Suppression, AIAA Journal of Aircraft, Vol. 41, No. 2, pp. 409-501. https://doi.org/10.2514/1.3281
- Bae, J. S., Kim, D. H., Yang, S. M. and Lee, I., 2002, Flutter Suppression of Wing/Store Model, Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 12, No. 7, pp. 493-501. https://doi.org/10.5050/KSNVN.2002.12.7.493
- Luo, Z., Chen, L., Yang, J., Zhang, Y. and Abdel-Malek, K., 2005, Compliant Mechanism Design Using Multi-objective Topology Optimization Scheme of Continuum Structures, Structural and Multidisciplinary Optimization, Vol. 30, No. 2, pp. 142-154. https://doi.org/10.1007/s00158-004-0512-y
- Kim, D.-K., Lee, J.-S. and Han, J.-H., 2011, Improved Aerodynamic Model for Efficient Analysis of Flapping-wing Flight, AIAA Journal, Vol. 49, No. 4, pp. 868-872. https://doi.org/10.2514/1.J050556
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