[1] Wright, J., and Cooper, J.J.A., "Introduction to Aircraft Aeroelasticity and Loads", 2nd Edition, Courier Dover Publications, New York, pp. 123-139, (2007).
[2] Krishnamurthy, T., and Mason, B., "Equivalent Plate Analysis of Aircraft Wing with Discrete Source Damage", 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference,14th AIAA/ASME/AHS Adaptive Structures Conference 7th, May 1-4, Newport, Rhode Island, USA, pp. 2218, (2006).
[3] Fung, Y.C., "An Introduction to the Theory of Aeroelasticity", 3rd Edition, Courier Dover Publications, New York, pp. 186-187, (2008).
[4] Kussner, H., "General Airfoil Theory", Report 19930094437, NACA TM-979, (1941).
[5] Watkins, C.E., Woolston, D.S., and Cunningham, H.J., "A Systematic Kernel Function Procedure for Determining Aerodynamic Forces on Oscillating or Steady Finite Wings at Subsonic Speeds", Report 118098417, NASA TR-R-48, (1959).
[6] Redman, M., and Rowe, W., "Prediction of Unsteady Aerodynamic Loadings Caused by Leading Edge and Trailing Edge Control Surface Motions in Subsonic Compressible Flow", Report 107297721, NASA CR-2543, (1975).
[7] Albano, E., and Rodden, W.P., "A Doublet-lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows", AIAA Journal, Vol. 7, pp. 279-285, (1969).
[8] Blair, M., "A Compilation of the Mathematics Leading to the Doublet Lattice Method", Report 116860505, WL-TR-92-3028, (1992).
[9] Rodden, W.P., Taylor, P.F., and McIntosh Jr, S.C., "Further Refinement of the Subsonic Doublet-lattice Method", Journal of Aircraft, Vol. 35, pp. 720-727, (1998).
[10] Ueda, T., and Dowell, E., "A New Solution Method for Lifting Surfaces in Subsonic Flow", AIAA Journal, Vol. 20, pp. 348-355, (1982).
[11] Hollowell, S.J., and Dugundji, J., "Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite/Epoxy Cantilevered Plates", Journal of Aircraft, Vol. 21, pp. 69-76, (1984).
[12] Lin, K.-J., Lu, P.-J., and Tarn, J.-Q., "Flutter Analysis of Cantilever Composite Plates in Subsonic Flow", AIAA Journal, Vol. 27, pp. 1102-1109, (1989).
[13] Koo, K., and Lee, I., "Aeroelastic Behavior of a Composite Plate Wing with Structural Damping", Computers and Structures, Vol. 50, pp. 167-176, (1994).
[14] Abdelrahmen, W., "Static and Dynamic Behaviour of Composite Swept Wings", M.Sc. Thesis, Department of Aerospace Engineering, Cairo University, Cairo, (1995).
[15] Dunn, P., and Dugundji, J., "Nonlinear Stall Flutter and Divergence Analysis of Cantilevered Graphite/Epoxy Wings", AIAA Journal, Vol. 30, pp. 153-162, (1992).
[16] Livne, E., and Li, W.-L., "Aeroservoelastic Aspects of Wing/Control Surface Planform Shape Optimization", AIAA Journal, Vol. 33, pp. 302-311, (1995).
[17] Lu, P.-J., and Huang, L.-J., "Flutter Suppression of Thin Airfoils using Active Acoustic Ecitations", AIAA Journal, Vol. 30, pp. 2873-2881, (1992).
[18] Na, Y.-H., and Shin, S., "Equivalent-plate Analysis for a Composite Wing with a Control Surface", Journal of Aircraft, Vol. 50, pp. 853-862, (2013).
[19] Abbas, M.K., Negm, H.M., and Elshafei, M.A., "Flutter and Divergence Characteristics of Composite Plate Wing", International Conference on Aerospace Sciences and Aviation Technology, May 28-30, Cairo, Egypt, pp. 1-21, (2013).
[20] Jian, T., Changchuan, X., and Chao, Y., "Flutter Analysis of Aircraft Wing using Equivalent-plate Models with Orthogonal Polynomials", Transactions of Nanjing University of Aeronautics and Astronautics, Vol. 32, pp. 5, (2015).
[21] Saeed, S., and Salman, S., "Flutter Analysis of Hybrid Metal-composite Low Aspect Ratio Trapezoidal Wings in Supersonic Flow", Chinese Journal of Aeronautics, Vol. 30, pp. 196-203, (2017).
[22] Babin, T., and Sangeetha, N., "Flutter Analysis of Supersonic Low Aspect Ratio Composite Wings using FSI Methodology", Advances in Manufacturing Processes, September 11, Singapore, pp. 361-372, (2019).
[23] He, X., Song, Z., Wu, Z., and Liu, F., "Aeroelastic Testing for Freeplay Induced Limit Cycles of Flexible Wing-aileron System", AIAA Scitech 2020 Forum, January 6-10, Orlando, USA, pp. 21-31, (2020).
[24] Pohly, J.A., Zhang, M.R., and Zhang, S., "Wing Flutter Analysis using Computational Fluid-structure Interaction Dynamics", ASME 2021 Fluids Engineering Division Summer Meeting, August 10–12, Virtual, Online, pp. 1-8, (2021).
[25] Kapania, R.K., and Lovejoy, A.E., "Free Vibration of Thick Generally Laminated Cantilever Quadrilateral Plates", AIAA Journal, Vol. 34, pp. 1474-1486, (1996).
[26] Kapania, R.K., and Liu, Y., "Static and Vibration Analyses of General Wing Structures using Equivalent-plate Models", AIAA Journal, Vol. 38, pp. 1269-1277, (2000).
[27] Lovejoy, A.E., "Natural Frequencies and an Atlas of Mode Shapes for Generally-laminated, Thick, Skew, Trapezoidal Plates", M.Sc. Thesis, Department of Aerospace Engineering, University of Virginia, Virginia, (1994).
[28] Crawley, E.F., Curtiss, H.C., Peters, D.A., Scanlan, R. H., and Sisto, F., "A Modern Course in Aeroelasticity", 4th Edition, Springer, New York, pp. 246, (1995).
[29] Bisplinghoff, R.L., Ashley, H., and Halfman, R.L., "Aeroelasticity", 2nd Edition, Courier Corporation, New York, pp. 545-551, (2013).
[30] Na, Y.-H., Kim, J.-H., and Shin, S.-J., "Vibration Analyses of an Equivalent Plate Wing with an External Store", The Aeronautical Journal, Vol. 118, pp. 1090-1098, (2014).