Impact, Blast and Crashworthiness

  1. Rizzo, F; D'Agostino, T; Cuomo, S; Pinto, F; Meo, M; High-velocity impact investigation on thermoplastic polyurethane/CFRP T-stiffened panel ,Materials Today: Proceedings ,2020 ,Elsevier

  2. Pinto, F; Meo, M; Design and manufacturing of a novel shear thickening fluid composite (STFC) with enhanced out-of-plane properties and damage suppression , Applied Composite Materials , 24 , 3 , 643-660 , 2017 , Springer Netherlands

  3. Ginzburg, D; Pinto, F; Iervolino, O; Meo, M; Damage tolerance of bio-inspired helicoidal composites under low velocity impact , Composite Structures , 161 , 187-203 , 2017 , Elsevier

  4. Pinto, F; Carotenuto, G; Meo, Michele; Preparation and thermomechanical characterisation of graphene nanoplatelets/low-density polyethylene composites Journal of Thermoplastic Composite Materials 28 6 745-761 2015 SAGE Publications

  5. M Guida, F Marulo, M Meo, S Russo, ‘Certification by birdstrike analysis on C27J fullscale ribless composite leading edge’, International Journal of Impact Engineering, Volume 54, April 2013, pp. 105–113

  6. M. Meo, F. Marulo, M. Guida S. Russo, ‘Shape memory alloy hybrid composites for improved impact properties for aeronautical applications’, Composite Structures, Composite Structures, 2013, pp. 756-766.

  7. Guida, M., Marulo, F. , Meo, M., & Russo, S. (2012). Experimental tests analysis of fiber metal laminate under birdstrike. Mechanics of Advanced Materials and Structures, 19(5), pp. 376-395.

  8. Dolce, F. , Meo, M., Wright, A., French, M., & Bernabei, M. (2011). Hybrid S2/Carbon epoxy composite armours under blast loads. Applied Composite Materials, 19(3-4), pp. 349-362.

  9. Guida, M., Marulo, F. , Meo, M., Grimaldi, A., & Olivares, G. (2011). SPH - Lagrangian study of bird impact on leading edge wing. Composite Structures, 93(3), pp. 1060-1071.

  10. Tsartsaris, N., Meo, M., Dolce, F., Polimeno, U., Guida, M., & Marulo, F. (2011). Low-velocity impact behavior of fiber metal laminates. Journal of Composite Materials, 45(7), pp. 803-814.

  11. Dolce, F., Meo, M., Wright, A., & French, M. (2010). Structural response of laminated composite plates to blast load. Plastics, Rubber and Composites: Macromolecular Engineering, 39(3-5), pp. 180-188.

  12. Guida, M., Marulo, F., Polito, T. , Meo, M., & Riccio, M. (2009). Design and testing of a fiber-metal-laminate bird-strike-resistant leading edge. Journal of Aircraft, 46(6), pp. 2121-2129.

  13. Guida, M. , Meo, M., Riccio, M., & Marulo, F. (2008). Analysis of bird impact on a composite tailplane leading edge. Applied Composite Materials, 15(4-6), pp. 241-257.

  14. Meo, M., Vignjevic, R., & Marengo, G. (2005). The response of honeycomb sandwich panels under low-velocity impact loading. International Journal of Mechanical Sciences, 47, pp. 1301-1325.

  15. Meo, M., Morris, A., Vignjevic, R., & Marengo, G. (2003). Numerical simulations of low-velocity impact on an aircraft sandwich panel. Composite Structures, 62, pp. 353-360.

  16. Vignjevic, R. , & Meo, M. (2002). A new concept for a helicopter sub-floor structure crashworthy in impacts on water and rigid surfaces. International Journal of Crashworthiness, 7, pp. 321-330.