[[1]] Hodges DH, Dowell EH (1974) Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. (No. Naca-A-5711(.
[2] Arafat HN (1999) Nonlinear response of cantilever beams. Doctoral Dissertation, Virginia Polytechnic Institute and State University.
[3] Hodges DH (2003) Geometrically exact intrinsic theory for dynamics of curved and twisted anisotropic beams. AIAA J 41(6): 1131-1137.
[4] Reissner E (1973) On one-dimensional large-displacement finite-strain beam theory. Stud Appl Math 52(2): 87-95.
[5] Hegemier GA, Nair S (1977) A nonlinear dynamical theory for heterogeneous anisotropic elastic rods. AIAA J 15(1): 8-15.
[6] Hodges DH, Shang X, Cesnik CE (1996) Finite element solution of nonlinear intrinsic equations for curved composite beams. J Am Helicopter Soc 41(4): 313-321.
[7] Patil MJ, Hodges DH (2006) Flight dynamics of highly flexible flying wings. J Aircraft 43(6): 1790-1799.
[8] Chang CS, Hodges D (2009) Vibration characteristics of curved beams. J Mech Mater Struct 4(4): 675-692.
[9] Sotoudeh Z, Hodges DH (2009) Nonlinear aeroelastic analysis of joined-wing aircraft with intrinsic equations. In 50th Structures, Structural Dynamics, and Materials Conference, Palm Springs, CA, AIAA Paper.
[[1]0] Shams S, Lahidjani MS, Haddadpour H (2008) Nonlinear aeroelastic response of slender wings based on Wagner function. Thin Wall Struct, 46(11): 1192-1203.
[1[1]] Dunn P, Dugundji J (1992) Nonlinear stall and divergence analysis of cantilevered graphite/epoxy wing. AIAA J 30(1): 153-162.
[12] Tang D, Dowell EH (2001) Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings. AIAA J 39(8): 1430-1441.
[[1]3] Jian Z, Jinwu X (2009) Nonlinear aeroelastic response of high-aspect-ratio flexible wings. Chinese J Aeronaut 22(4): 355-363.
[[1]4] Patil MJ (1999) Nonlinear aeroelastic analysis flight dynamics and control of a complete aircraft. Georgia Institute of Technology.
[[1]5] Barmby JG, Cunningham HJ, Garrick IE (1950) Study of effects of sweep on the flutter of cantilever wings. (No. Naca-TR-1014).
[[1]6] Molyneux WG, Hall H (1957) The aerodynamics effects of aspect ratio and sweepback on wing flutter. (A.R.C-TR).
[[1]7] Lottati I (1985) Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing. J Aircraft 22(11): 1001-1007.
[[1]8] Karpouzian G, Librescu L (1996) Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings. AIAA J 34(4): 786-794.
[[1]9] Mazidi A, Fazelzadeh SA (2010) Flutter of a swept aircraft wing with a powered engine. J Aerospace Eng 23(4): 243-250.
[20] مروج ح، آموزگار م، شاهوردی ح (1396) تحلیل ناپایداری فلاتر بالهای دارای زاویه پس گرایی با استفاده از معادلات کاملاً ذاتی. نشریه مهندسی مکانیک امیرکبیر 794-785 :(4)49.
[2[1]] Amoozgar MR, Shahverdi H (2016) Analysis of nonlinear fully intrinsic equations of geometrically exact beams using generalized differential quadrature method. ACTA Mech 227(5): 1265-1277.
[22] Hodges DH (1990) A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams. Int J Solids Struct 26(11): 1253-1273.
[23] Beedy J, Barakos G (2002) Non-linear analysis of stall flutter based on the ONERA Aerodynamic model. Aerospace Engineering Report 0205b.
[24] O'Reilly OM (2008) Intermediate dynamics for engineers: a unified treatment of newton-euler and lagrangian mechanics. Cambridge University Press.
[25] Patil MJ, Hodges DH, Cesnik CE (2001) Limit-cycle oscillations in high-aspect-ratio wings. J Fluid Struct 15(1): 107-132.
[26] Chang CS (2006) Vibration and aeroelastic analysis of highly flexible HALE aircraft. Doctoral Dissertation, Georgia Institute of Technology.