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Dept. of Mechanical and Aerospace Engineering, Polytecnico di Torino, Italy
Selected Publications:
Romeo G., Frulla G. (1992) : Buckling and postbuckling behaviour of anisotropic plates under combined biaxial compression and shear loads. ECCM Composite Testing and Standardisation (Amsterdam 09/92).
G. Romeo, G. Frulla and M. Busto, Nonlinear Angle of Twist of Advanced Composite Wing Boxes Under Pure Torsion, Journal of Aircraft, 31(6) (1994).
Romeo G, Frulla G. Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads. Int J Solids Struct 1994;31(6):763–783.
Romeo G., and Frulla G., “Nonlinear Analysis of Graphite/Epoxy Wing Boxes under Pure Bending Including Lateral Pressure”, Journal of Aircraft, Vol. 32, No. 6, 1995, pp. 1375-1381.
Romeo G., and Frulla G., “Postbuckling Behaviour of Graphite/Epoxy Wing Boxes Panels under Pure Torsion”, Proceedings of the 20th Congress of the International Council of Aeronautical Sciences (ICAS), Washington (USA), 1996, Vol. I, pp. 1156-1166.
Antona, E. and Frulla, G. (2001), “Cicala's asymptotic approach to the linear shell theory”,Composite Structures,52, 13–26.
Romeo G., and Frulla G, “Postbuckling Behaviour of Graphite/Epoxy Stiffened Panels with Initial Imperfections subjected to Eccentric Biaxial Compression Loading”, International Journal of Non-Linear Mechanics, Vol. 32, No. 6, 1997, pp. 1017-1033. Romeo G., and Ferrero G., “Analytical/Experimental Behavior of Anisotropic Rectangular Panels under Linearly Varying Combined Loads”, AIAA Journal, Vol. 39, No. 5, 2001, pp. 932-941.
Frulla G., “Buckling and Postbuckling Behavior of Anisotropic Rectangular Panels under Linearly Varying Combined Loads”, International Journal of Mechanics and Control, Vol.6, No.1, 2005, pp. 13-20.
Frulla G., “Experimental Behavior of Damaged Anisotropic Rectangular Panels under Cyclic Compressive Loads”, Proceedings of the XVIII AIDAA National Congress , 2005.
Frulla G., “Structural Behavior of Damaged Anisotropic Stiffened Panels under Compressive Loads”, Proceedings of the 25th ICAS Congress, 2006.
Romeo, G., and Frulla, G., “Post-Buckling Behaviour of Graphite/Epoxy Stiffened Panels with Initial Imperfections Subjected to Eccentric Biaxial Compression Loading,” International Journal of Non-Linear Mechanics, Vol. 32, No. 6, 1997, pp. 1017–1033.
Chiara Bisagni, Vittorio Giavotto, Giulio Romeo, Giacomo Frulla, Daniele Fanteria and Agostino Lanciotti, “Research activities on buckling of composite structures in Italy”, AIAA Paper 2009-2349, 50th AIAA Structures, Structural Dynamics and Materials Conference, 4-7 May 2009, Palm Springs, California
M. Battipede, E. Cestino, G. Frulla, S. Gerussi and P. Gili, “Innovative aircraft aeroelastic modeling and control”, 27th International Congress of the Aeronautical Sciences (ICAS 2010), 2010
Borello F, Cestino E, Frulla G (2010) Structural uncertainty effect on classical wing flutter characteristics. J Aerosp Eng 23(4):327–338
Cestino, E., Frulla, G., Duella, R., Piana, P. et al., "Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams," SAE Technical Paper 2017-01-2059, 2017, doi:10.4271/2017-01-2059.
Luca Praticò, Joel Galos, Enrico Cestino, Giacomo Frulla and Pier Marzocca, “Experimental and numerical vibration analysis of plates with curvilinear sub-stiffeners”, Engineering Structures, Vol. 209, Article 109956, 15 April 2020
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