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doi:10.1016/j.ijsolstr.2005.07.045
www-mech.eng.cam.ac.uk/profiles/fleck/papers/215.pdf20 Jul 2007: 0a. 0 0.2 0.4 0.6 0.80. 6. 12. 18. 24. b. ... 12. 18. 24. b. 0 0.02 0.04 0.06 0.080. 10. 20. -
doi:10.1016/j.ijfatigue.2006.11.013
www-mech.eng.cam.ac.uk/profiles/fleck/papers/224.pdf31 Mar 2007: Acta Mater 1999;47(8):2511–24. [7] Sugimura Y, Rabiei A, Evans AG, Harte A-M, Fleck NA.Compression fatigue of a cellular Al alloy. -
doi:10.1016/j.jmps.2006.08.004
www-mech.eng.cam.ac.uk/profiles/fleck/papers/227.pdf26 Jan 2007: Received 24 April 2006; received in revised form 18 August 2006; accepted 24 August 2006. ... sA 0 and sB 2:9T. r̄2. (24). We shall show below in a case study on the centre-cracked panel subjected to uniaxialtension that the large negative T-stress is -
Paper.dvi
www-mech.eng.cam.ac.uk/profiles/fleck/papers/238.pdf1 Mar 2007: thereby obtain399. KIIC = 0.047ρ1.5σf. (24). This is in reasonable agreement with the values for (D, d) as listed in Table 3400. ... toughness for any lattice by462. KIC =KIC(R/). KIC(0)(34). 24. where KIC(R/) is the mode I fracture toughness of the -
1 arwwsscSort u�bar G JssJnaA 3 G. J. McShane ...
www-mech.eng.cam.ac.uk/profiles/fleck/papers/221.pdf1 May 2007: 24 mm. The sandwich beams comprise identical front and backace-sheets of thickness h = 8 mm and a core of depth c360 mm. ... In addition to these sandwich beams, a reference monolithicsteel beam of thickness d = 24.0 mm mass per unit area equal tothat of
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