Hoskins, B.C. and Baker, A.A., “Composite Materials in Aircraft Structures”, AIAA Educ. Series, Renton, VA. 1986,
 Qin, Z., “Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams–Dynamics, Stability and Control”, Virginia Polytechnic .Institute and StateUniversity, Ph.D. dissertation, 2001
 Weisshaar, T.A., “Aeroelastic Tailoring-Creative Use of Unusual Materials”, AIAA Paper 87-97, AIAA/ASME/ASCE/AHS 28th Structures, Structural Dynamics and Materials Conference, April 9-10, 1987.
 Lazarus, K.B., Crawley, E.F. and Bohlmann, J.D, “Static Aeroelastic Control Using Strain Actuated Adaptive Structures” J. of Intelligent Material System and Structures, Vol. 2, July 1991, pp.386-410.
 Ehlers, S.M. and Weisshaar, T.A., “Static Aeroelastic Behaviour of an Adaptive Laminated Piezoelectric Composite Wing”, Proceeding of the AIAA/ASME/ASCE/AHS/
 ASC 31th Structures, Structural Dynamics and Materials Conference, Long Beach, CA, April 1990.
 Crawley, E.F, and Dugundji, J., “Frequency Determination and Nondimensionalization for Composite Cantilever Plates”, Journal of Sound and Vibration, Vol. 72, No. 1, 1980, pp. 1-10.
 Crawley, E.F., and Jensen, D.W., “Frequency Determination Techniques for Cantilevered Plates with Bending-Torsion Coupling” AIAA J., Vol. 22, 1984, pp.415-420.
 Kaza K.R.V., and Kielb, R.E., “Effects of Warping and Pretwist on Torsional Vibration of Rotating Beams” Transactions of ASME, J. of Applied Mechanics, Vol. 51, Dec., 1984, pp. 913-920.
 Librescu, L., and Song, O., “Behavior of Thin-Walled Beams Made of Advanced Composite Materials and Incorporating Non-Classical Effects”, Applied Mechanics Reviews, Vol. 44, No. 11, Part 2,1991, pp. 174-180.
 Timoshenko, S.P., “On the Transverse Vibrations of Bars of Uniform Cross Section” Philosophical Magazine, Series 6, Vol 43, 1922, pp. 125-131.
 Davies, R.M., “The Frequency of Transverse Vibration of a Loaded Fixed-Free Bar: IV The Effects of Shearing of the Bar” Philosophical Magazine, Series 7, Vol. 23, 1937, pp 1129-1145.
 Jacobsen, L.S., “Natural Frequencies of Uniform Cantilever Beams of Symmetrical Cross- Section” J. of Applied Mechanics, A-1, Vol. 5, 1938.
 Qin, Z., and Librescu, L., “Dynamic Aeroelastic Response of Aircraft Wings Modeled as Anisotropic Thin-Walled Beams” Journal of Aircraft, Vol. 40, No. 3, 2003.
 Haddadpour, H., Kouchakzadeh, M.A., and Shadmehri, F., “Aeroelastic instability of aircraft composite wings in an incompressible flow“, Composite Structure, Vol. 83, 2008, pp 93-99.
 Marzocca, P., Librescu, L., and Chiocchia, G., “Aeroelastic response of a 2-D airfoil in a compressible flow field and exposed to blast loading”, Aerospace Science and Technology, 2002, pp 259-272.
 Barmby, J. G., Cunningham, H. J., and Garrick, I. E., “Study of Effects of Sweep on the flutter of Cantilever Wing”, NACA TN-2121. 1950.