D.H. Hodges, E. Dowell, Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades, (1974).
 H.N. Arafat, Nonlinear response of cantilever beams, Virginia Tech, 1999.
 D.H. Hodges, Geometrically exact, intrinsic theory for dynamics of curved and twisted anisotropic beams, AIAA journal, 41(6) (2003) 1131-1137.
 E. Reissner, On One‐Dimensional Large‐Displacement Finite‐Strain Beam Theory, Studies in applied mathematics, 52(2) (1973) 87-95.
 G. Hegemier, S. Nair, A nonlinear dynamical theory for heterogeneous, anisotropic, elasticrods, AIAA Journal, 15(1) (1977) 8-15.
 D.H. Hodges, X. Shang, C.E. Cesnik, Finite element solution of nonlinear intrinsic equations for curved composite beams, Journal of the American Helicopter Society, 41(4) (1996) 313-321.
 M.J. Patil, D.H. Hodges, Flight dynamics of highly flexible flying wings, Journal of Aircraft, 43(6) (2006)1790-1799.
 C.-S. Chang, D. Hodges, Vibration characteristics of curved beams, Journal of Mechanics of Materials and Structures, 4(4) (2009) 675-692.
 Z. Sotoudeh, D. Hodges, Nonlinear aeroelastic analysis of joined-wing aircraft with fully intrinsic equations,in: 50th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics, and Materials Conference 17th AIAA/ASME/AHS Adaptive Structures Conference 11th AIAA No, 2009, pp. 2464.
 M.J. Patil, M. Althoff, Energy-consistent, Galerkin approach for the nonlinear dynamics of beams using intrinsic equations, Journal of Vibration and Control,17(11) (2011) 1748-1758.
 M.J. Patil, D.H. Hodges, Variable-order finite elements for nonlinear, fully intrinsic beam equations, Journal of Mechanics of Materials and Structures, 6(1) (2011) 479-493.
 J.G. Barmby, H.J. Cunningham, I. Garrick, Study of effects of sweep on the flutter of cantilever wings, (1951).
 W. Molyneux, H. Hall, The aerodynamic effects of aspect ratio and sweepback on wing flutter, Citeseer,1957.
 I. Lottati, Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing, Journal of Aircraft, 22(11) (1985) 1001-1007.
 G. Karpouzian, L. Librescu, Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings, AIAA journal, 34(4) (1996) 786-794.
 A. Mazidi, S. Fazelzadeh, Flutter of a swept aircraft wing with a powered engine, Journal of Aerospace Engineering, 23(4) (2009) 243-250.
 D.H. Hodges, A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams, International journal of solids and structures, 26(11)(1990) 1253-1273.
 C.-S. Chang, Vibration and aeroelastic analysis of highly flexible HALE aircraft, Georgia Institute of Technology,2006.
 H.A. Ardakani, T. Bridges, Review of the 3-2-1 euler angles: a yaw-pitch-roll sequence, Department of Mathematics, University of Surrey, Guildford GU2 7XH UK, Tech. Rep, (2010).
 D.A. Peters, S. Karunamoorthy, W.-M. Cao, Finite state induced flow models. I-Two-dimensional thin airfoil, Journal of Aircraft, 32(2) (1995) 313-322.
 M.J. Patil, Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft, Citeseer,1999.