A structural member for a vehicle body, comprising: a plate member; a facia member connected to the plate member, the facia member and the plate member defining therebetween a cavity; and an energy absorbing device (100, 200, 300, 400, 500, 600, 700, 800, 900, 1000) supported within the cavity, the energy absorbing device, comprising: a honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) having a plurality tubes (104, 204, 304, 404, 504, 604, 704, 804, 904, 1004) stacked transversely with one another along a longitudinal axis, the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) comprising: an inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) arranged along the longitudinal axis and having an inboard portion bending stiffness; and an outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) arranged outboard of the longitudinal axis and coupled to the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002), the outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) having an outboard portion bending stiffness, wherein the outboard portion bending stiffness of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) is greater than the inboard portion bending stiffness of the honeycomb body; and wherein the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) abuts the plate member. a plate member; a facia member connected to the plate member, the facia member and the plate member defining therebetween a cavity; and an energy absorbing device (100, 200, 300, 400, 500, 600, 700, 800, 900, 1000) supported within the cavity, the energy absorbing device, comprising: a honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) having a plurality tubes (104, 204, 304, 404, 504, 604, 704, 804, 904, 1004) stacked transversely with one another along a longitudinal axis, the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) comprising: an inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) arranged along the longitudinal axis and having an inboard portion bending stiffness; and an outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) arranged outboard of the longitudinal axis and coupled to the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002), the outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) having an outboard portion bending stiffness, wherein the outboard portion bending stiffness of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) is greater than the inboard portion bending stiffness of the honeycomb body; and wherein the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) abuts the plate member. a honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) having a plurality tubes (104, 204, 304, 404, 504, 604, 704, 804, 904, 1004) stacked transversely with one another along a longitudinal axis, the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) comprising: an inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) arranged along the longitudinal axis and having an inboard portion bending stiffness; and an outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) arranged outboard of the longitudinal axis and coupled to the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002), the outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) having an outboard portion bending stiffness, wherein the outboard portion bending stiffness of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) is greater than the inboard portion bending stiffness of the honeycomb body; and wherein the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) abuts the plate member. an inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) arranged along the longitudinal axis and having an inboard portion bending stiffness; and an outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) arranged outboard of the longitudinal axis and coupled to the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002), the outboard portion (112, 212, 312, 412, 512, 712, 812, 912, 1012) having an outboard portion bending stiffness, wherein the outboard portion bending stiffness of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) is greater than the inboard portion bending stiffness of the honeycomb body; and wherein the inboard portion (108, 208, 308, 408, 508, 708, 808, 908, 1008) of the honeycomb body (102, 202, 302, 402, 502, 602, 702, 802, 902, 1002) abuts the plate member.