'Fig. 41. Curves of constant relative resolved shear stress for the ten likely secondary slip systems. The numbering of the systems is as Fig. 1 and the relative resolved shear stress is calculated as a fraction of the resolved shear stress on the system BIV, i.e. the primary system, for orientations in the standard triangle' from "Work Hardening of Metals" by L. M. Clarebrough and M. E. Hargreaves, Progress in Metal Physics Vol. 8, p.66.

10 poster charts

'Fig. 41. Curves of constant relative resolved shear stress for the ten likely secondary slip systems. The numbering of the systems is as Fig. 1 and the relative resolved shear stress is calculated as a fraction of the resolved shear stress on the system BIV, i.e. the primary system, for orientations in the standard triangle' from "Work Hardening of Metals" by L. M. Clarebrough and M. E. Hargreaves, Progress in Metal Physics Vol. 8, p.66.

10 charts 350mm x 300mm prepared for photographic reproduction

'Fig. 41. Curves of constant relative resolved shear stress for the ten likely secondary slip systems. The numbering of the systems is as Fig. 1 and the relative resolved shear stress is calculated as a fraction of the resolved shear stress on the system BIV, i.e. the primary system, for orientations in the standard triangle' from "Work Hardening of Metals" by L. M. Clarebrough and M. E. Hargreaves, Progress in Metal Physics Vol. 8, p.66.

10 charts, drafts 350mm x 300mm

Schematic section of Calorimeter used for measuring energy stored in a metal during plastic deformation. From "The Determination of the Energy Stored in a Metal during Plastic Deformation" by L. M. Clarebrough, M. E. Hargreaves, D. Michell and G. W. West. (Figure 1) Proceedings of the Royal Society, A, 215, 1952, pp 507-524

Schematic diagram of the electrical circuits of the apparatus used for measuring the stored energy in a deformed metal. From "The Determination of the Energy Stored in a Metal during Plastic Deformation" by L. M. Clarebrough, M. E. Hargreaves, D. Michell and G. W. West. (Figure 4) Proceedings of the Royal Society, A, 215, 1952, pp 507-524

Power difference (vetical axis) as a function of time (horizontal axis) for specimens (of copper) deformed various amounts in torsion. The curves fom left to right are for values of nd/l decreasing from 3.03 to 0.47, from "The Determination of the Energy Stored in a Metal during Plastic Deformation" by L. M. Clarebrough, M. E. Hargreaves, D. Michell and G. W. West. (Figure 8) Proceedings of the Royal Society, A, 215, 1952, pp 507-524

Diagram showing stored energy (vertical axis) versus work done in twisting (horizontal axis) and recrystallization temperature (vertical axis) versus work done in twisting for several copper specimens, from "The Determination of the Energy Stored in a Metal during Plastic Deformation" by L. M. Clarebrough, M. E. Hargreaves, D. Michell and G. W. West. (Figure 5) Proceedings of the Royal Society, A, 215, 1952, pp 507-524

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.

Probably related to War work done in the Department of Metallurgy concerning the failures of the cooling systems in Spitfire aircraft operating in the Darwin area during World War II.