[1] Alibeigloo, A., Shakeri, M., and Kari, M., “Free Vibration Analysis of Antisymmetric Laminated Rectangular Plates With Distributed Patch Mass Using Third-Order Shear Deformation Theory” Ocean Engineering, Vol. 35, No. 9, pp. 183-190, 2008.
[2] Farhadi, S. and Hosseini-Hashemi, S., “Effect of a Bonded Patch on Aeroelastic Behavior of Cantilevered Plates” Journal of Applied Mathematics, vol. 20, No. 14, pp. 13-20, 2010.
[3] Gorman, D., “Free Vibration Analysis of Cantilever Plates by the Method of Superposition” Journal of Sound and Vibration, Vol. 49, No. 10, pp. 453-467, 1976.
[4] Boay, C. G., “Frequency Analysis of Rectangular Isotropic Plates Carrying a Concentrated Mass,” Computers & structures, Vol. 56, No. 14, pp. 39-48, 1995.
[5] Kopmaz, O. and Telli, S., “Free Vibrations of a Rectangular Plate Carrying a Distributed Mass” Journal of Sound and Vibration, Vol. 251, No. 6, pp. 39-57, 2002.
[6] Wong, W., “The Effects of Distributed Mass Loading on Plate Vibration Behavior” Journal of Sound and Vibration, Vol. 252, No. 11, pp. 577-583, 2002.
[7] Alashti, R. A. and Alibakhshi, R., “Free Vibration of Simply Supported Rectangular Composite Plates With Patch Mass” Computers & structures, Vol. 32, No. 8, pp. 3-48, 2012.
[8] Alibakhshi, R., “The Effect of Anisotropy on Free Vibration of Rectangular Composite Plates with Patch Mass” International Journal of Engineering, Vol. 25, No. 3, pp. 223-232, 2012.
[9] Alibakhshi, R. and Alashti, R. A., “Vibration Analysis of Laminated Composite Plates Carrying Rotating Circular Mass,” International Journal of Advanced Design and Manufacturing Technology, Vol. 7, No. 11, pp. 1-9, 2014.
[10] Jordan PF. “The physical nature of panel flutter”. Aero Digest. Vol. 34, No. 8, 1956.
[11] Dowell, EH. Panel flutter., “a review of the aeroelastic stability of plates and shells” AIAA J, Vol. 8, No. 3, pp. 385–99, 1970.
[12] Bismarck-Nasr, MN. “Finite element analysis of aeroelasticity of plates and shells”. Appl Mech Rev, Vol.45, No. 12, pp. 461–82, 1992.
[13] Bismarck-Nasr MN. “Finite elements in aeroelasticity of plates and shells”. Appl Mech Rev, Vol.49, No. 10, pp. 17–24, 1996.
[14] Durvasula S. Flutter of simply supported parallelogrammic flat panels in supersonic flow. AIAA J; Vol. 5, pp. 1668–73, 1967.
[15] Kariappa V, Somashekar BR, Shaw CG., “Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flow”, AIAA J, Vol. 8, pp. 2017–22, 1970.
[16] Sander G, Bon C, Geradin M., “Finite element analysis of a supersonic panel flutter”, Int J Numer Meth Eng.Vol.7, pp. 379–94, 1973.
[17] Srinivasan RS, Babu BJC., “Flutter analysis of cantilevered quadrilateral plates” J Sound Vib, Vol.98, No. 1, pp. 45–53, 1985.
[18] Srinivasan RS, Babu BJC., “Free vibration and flutter of laminated quadrilateral plates”, Comput Struct, Vol. 27, pp. 297–304, 1987.
[19] Farhadi S. S. Hosseini-Hashemi, “Flutter stabilization of cantilevered plates using a bonded patch,” Vol.219, pp. 241–254, 2011.
[20] Dowell, E. and Ye, W., “Limit cycle oscillation of a fluttering cantilever plate,” AIAA journal, Vol. 29, No. 5, pp. 1929-1936, 1991.
[21] Christensen, R. M., “Mechanics of composite materials: Courier Corporation,” Krieger Publishing Company, Florida, 2012.
[22] Sivakumara, K., “Natural frequencies of symmetrically laminated rectangular plates with free edges,” Composite structures, Vol. 7, No. 8, pp. 191-204, 1987.
[23] In, L. and Jung-Jin, L., “Vibration analysis of composite wing with tip mass using finite elements,” Computers & structures, Vol. 47, No. 2, pp. 495-504 1993.
[25] Mei, C., Abdel-Motagaly, K. and Chen, R., “Review of nonlinear panel flutter at supersonic and hypersonic speeds”, Appl.Mech. Rev. Vol 52, pp.416–421, 1999.
[26] Singha, M. K. and Ganapathi, M., “parametric study on supersonic flutter behavior of laminated composite skew flat panels”, Composite Structures, Vol 69, No. 9. pp. 55–63, 2005.