Mr. Edwards et Cl. Owen, THE TEARING OF PETALLED HOLES IN 2014-T651 ALUMINUM-ALLOY PRODUCED BYEXPLOSIONS AND ITS POSSIBLE CONTRIBUTION TO THE LOSS OF AIRCRAFT BY SABOTAGE, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 209(G1), 1995, pp. 53-63
Petalled holes were formed in thin 2014-T651 aluminium alloy sheet by
blast, explosively formed projectiles and shaped charges, as well as b
y explosives placed directly on the sheet. Tensile testing of the shee
ts containing the various holes showed no macroscopic plasticity. Anal
ysis of the lengths of petalled cracks produced by 1.26 g charges of a
n RDX-wax explosive in direct contact with a sheet, acting as a diaphr
agm in a canister, showed that these were increased by 50 per cent if
the canister was pressurized to 0.6 MPa (6 bar), indicating that the l
ength of petalled cracks produced by an explosion was affected by the
stress applied to the thin sheet. Calculations showed that the strain
energy in the diaphragm was 17.5 J, while the energy required to produ
ce the extra cracking was estimated to be 57 J, assuming that the work
required to extend the crack is 0.1 MJ/m(2) This suggested that the e
nergy stored in the gas, as well as that elastically stored in the dia
phragm, was used to extend the cracks. The lengths of petalled cracks
produced by 55 g charges of the RDX-wax explosive at 400 mm stand-off
were substantially less than those produced by the 1.26 g charges plac
ed in contact with the sheet, indicating the beneficial effect of the
attenuation of the blast wave by stand-off and the greater damage caus
ed by the presence of explosives in contact with or very close to the
sheet.