Publications by Dr B.P. RussellJump to: Article Number of items: 10.
ArticlePark, S and Russell, BP and Deshpande, VS and Fleck, NA (2012) Dynamic compressive response of composite square honeycombs. Composites Part A: Applied Science and Manufacturing, 43. pp. 527-536. ISSN 1359-835X Kazemahvazi, S and Russell, BP and Zenkert, D (2012) Impact of carbon fibre/epoxy corrugated cores. Composite Structures. ISSN 0263-8223 Kazemahvazi, S and Russell, BP and Zenkert, D (2012) Impact of carbon fibre/epoxy corrugated cores. Composite Structures, 94. pp. 3300-3308. ISSN 0263-8223 Russell, BP and Liu, T and Fleck, NA and Deshpande, VS (2012) The soft impact of composite sandwich beams with a square-honeycomb core. International Journal of Impact Engineering, 48. pp. 65-81. ISSN 0734-743X Park, S and Russell, BP and Deshpande, VS and Fleck, NA (2011) Dynamic compressive response of composite square honeycombs. Composites Part A: Applied Science and Manufacturing. ISSN 1359-835X Russell, BP and Liu, T and Fleck, NA and Deshpande, VS (2011) Quasi-static three-point bending of carbon fiber sandwich beams with square honeycomb cores. Journal of Applied Mechanics, Transactions ASME, 78. ISSN 0021-8936 Russell, BP and Liu, T and Fleck, NA and Deshpande, VS (2011) The soft impact of composite sandwich beams with a square-honeycomb core. International Journal of Impact Engineering. ISSN 0734-743X Russell, BP and Malcom, A and Wadley, HNG and Deshpande, VS (2010) DYNAMIC COMPRESSIVE RESPONSE OF COMPOSITE CORRUGATED CORES. J MECH MATER STRUCT, 5. pp. 477-493. ISSN 1559-3959 Côté, F and Russel, BP and Deshpande, VS and Fleck, NA (2009) The through-thickness compressive strength of a composite sandwich panel with a hierarchical square honeycomb sandwich core. Transactions of the ASME, Journal of Applied Mechanics, 76. 061004-. ISSN 0021-8936 Russell, BP and Deshpande, VS and Wadley, HNG (2008) Quasistatic deformation and failure modes of composite square honeycombs. Journal of the Mechanics of Materials and Structures, 3. pp. 1315-1340. |
