[1] Hoskins, B.C. and Baker, A.A., “Composite Materials in Aircraft Structures”, AIAA Educ. Series, Renton, VA. 1986,
[2] 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
[3] 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.
[4] 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.
[5] Ehlers, S.M. and Weisshaar, T.A., “Static Aeroelastic Behaviour of an Adaptive Laminated Piezoelectric Composite Wing”, Proceeding of the AIAA/ASME/ASCE/AHS/
[6] ASC 31th Structures, Structural Dynamics and Materials Conference, Long Beach, CA, April 1990.
[7] 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.
[8] 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.
[9] 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.
[10] 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.
[11] Timoshenko, S.P., “On the Transverse Vibrations of Bars of Uniform Cross Section” Philosophical Magazine, Series 6, Vol 43, 1922, pp. 125-131.
[12] 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.
[13] Jacobsen, L.S., “Natural Frequencies of Uniform Cantilever Beams of Symmetrical Cross- Section” J. of Applied Mechanics, A-1, Vol. 5, 1938.
[14] 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.
[15] 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.
[16] 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.
[17] 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.
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