[1] Pourshamsi, H., Mazidi, A., & Fazelzadeh, S. A. (2015). Flutter analysis of an aircraft wing carrying, elastically, an external store. Modares Mechanical Engineering, 15(1), 49-58.
[2] Wright, J. R., & Cooper, J. E. (2008). Introduction to aircraft aeroelasticity and loads. John Wiley & Sons.
[3] Peters, D. A., Karunamoorthy, S., & Cao, W. M. (1995). Finite state induced flow models part I: Two-dimensional thin airfoil. Journal of Aircraft, 32(2), 313-322.
[4] Peters, D. A. (2008). Two-dimensional incompressible unsteady airfoil theory—an overview. Journal of Fluids and Structures, 24(3), 295-312.
[5] Bisplinghoff, R. L., Ashley, H., & Halfman, R. L. (1955). Aeroelasticity, Addison-Weslej' Publishing Company.
[6] Azimi, S. M. H., Mazidi, A., & Azadi, M. (2017). Active control of an elastic beam with external mass under the thrust force. Presented at the Sixteenth International Conference of Iranian Aerospace Society(AERO2017), Print. (in Persian)
[7] Peng, X. Q., Lam, K. Y., & Liu, G. R. (1998). Active vibration control of composite beams with piezoelectrics: a finite element model with third order theory. Journal of Sound and Vibration, 209(4), 635-650.
[8] He, X. Q., Ng, T. Y., Sivashanker, S., & Liew, K. M. (2001). Active control of FGM plates with integrated piezoelectric sensors and actuators. International journal of solids and structures, 38(9), 1641-1655.
[9] Yang, Y., Ju, C., & Soh, C. K. (2003). Analytical and semi-analytical solutions for vibration control of a cantilevered column using a piezoelectric actuator. Smart Materials and Structures, 12(2), 193-199.
[10] Kim, H. W., & Kim, J. H. (2005). Effect of piezoelectric damping layers on the dynamic stability of plate under a thrust. Journal of Sound and Vibration, 284(3), 597-612.
[11] Fazelzadeh, S. A., & Azadi, M. (2007). Active Nonlinear Aeroelastic Control for Damping Vibration of a Tank Attached to the Wing. Presented at the Amirkabir university of technology: Fifteenth Annual Mechanical Conference (ISME2007). Print. (in Persian)
[12] Song, Z. G., & Li, F. M. (2011). Active aeroelastic flutter analysis and vibration control of supersonic beams using the piezoelectric actuator/sensor pairs. Smart Materials and Structures, 20(5), 55-68.
[13] Song, Z. G., & Li, F. M. (2012). Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate. Composite Structures, 94(2), 702-713.
[14] Li, F. M. (2012). Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material. International Journal of Engineering Science, 51, 190-203.
[15] Azadi, V., Azadi, M., Fazelzadeh, S. A., & Azadi, E. (2014). Active control of an fgm beam under follower force with piezoelectric sensors/actuators. International Journal of Structural Stability and Dynamics, 14(02), 1350-1363.
[16] Fazelzadeh, S. A., Azadi, M., & Azadi, E. (2017). Suppression of nonlinear aeroelastic vibration of a wing/store under gust effects using an adaptive-robust controller. Journal of Vibration and Control, 23(7), 1206-1217.
[17] Mazidi, A. (2011). Critical and post-critical behavior analysis of elastic aircraft wings subjected to non-conservative loads (PHD thesis). Shiraz University Faculty of Mechanical Engineering.
[18] Hodges, D. H., & Dowell, E. H. (1974). Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades.
[19] Mazidi, A., & Fazelzadeh, S. A. (2011). Aeroelastic modeling and flutter prediction of swept wings carrying twin powered engines. Journal of Aerospace Engineering, 26(3), 586-593.
[20] Hodges, D. H., & Pierce, G. A. (2011). Introduction to structural dynamics and aeroelasticity (Vol. 15). cambridge university press.
[21] Goland, M., & Luke, Y. L. (1948). The flutter of a uniform wing with tip weights. Journal of Applied Mechanics, 15(1), 13-20.
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