Series 6 - Graphic Materials (Oversize)


Date Range1959
ProvenanceMaxwell Edgar Hargreaves
Description

Posters, art work for publications


Inventory Listing

6-1 Fig. 41

'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

Creator Maxwell Edgar Hargreaves
Date range 1959    Quantity 1 file
Inventory Identifier 6-1 Series 6
6-2 Fig. 41

'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

Creator Maxwell Edgar Hargreaves
Date range 1959    Quantity 1 file
Inventory Identifier 6-2 Series 6
6-3 Fig. 41

'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

Creator Maxwell Edgar Hargreaves
Date range 1959    Quantity 1 file
Inventory Identifier 6-3 Series 6
6-4 Schematic section of Calorimeter used for measuring energy stored in a metal during plastic deformation

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

Creator Maxwell Edgar Hargreaves
Date range 1952    Quantity 1 file
Inventory Identifier 6-4 Series 6
6-5 Schematic diagram of the electrical circuits of the apparatus used for measuring the stored energy in a deformed metal

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

Creator Maxwell Edgar Hargreaves
Date range 1952    Quantity 1 file
Inventory Identifier 6-5 Series 6
6-6 Diagram

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

Creator Maxwell Edgar Hargreaves
Date range 1952    Quantity 1 file
Inventory Identifier 6-6 Series 6
6-7 Diagram

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

Creator Maxwell Edgar Hargreaves
Date range 1952    Quantity 1 file
Inventory Identifier 6-7 Series 6
6-8 Oil Circulation Diagram - Hercules VI, XVI & XVII Air Diagram 2585, Sheet No. 1 [of 4]

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.

Creator Maxwell Edgar Hargreaves
Date range September 1943    Quantity 1 file
Inventory Identifier 6-8 Series 6
6-9 Oil Circulation Diagram - Hercules VI, XVI & XVII Air Diagram 2585, Sheet No. 3 [of 4]

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.

Creator Maxwell Edgar Hargreaves
Date range September 1943    Quantity 1 file
Inventory Identifier 6-9 Series 6
6-10 Oil Circulation Diagram - Hercules VI, XVI & XVII Air Diagram 2585, Sheet No. 4 [of 4]

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.

Creator Maxwell Edgar Hargreaves
Date range September 1943    Quantity 1 file
Inventory Identifier 6-10 Series 6
6-11 Merlin Aero-Engine, Two piece block, single stage, two speed supercharger type Air Diagram 2632, Sheet No. 1 [of 1]

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.

Creator Maxwell Edgar Hargreaves
Date range October 1943    Quantity 1 file
Inventory Identifier 6-11 Series 6
6-12 Merlin Aero-Engines, Two stage, Two speed, Supercharger and Intercooler Air Diagram 2577, Sheet No. 1 [of 1]

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.

Creator Maxwell Edgar Hargreaves
Date range June 1943    Quantity 1 file
Inventory Identifier 6-12 Series 6
6-13 Merlin Aero-Engines, Two stage, Two speed, Supercharger and Intercooler, Float chamber carburettor Air Diagram 4157, Sheet No. 1 [of 1]

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.

Creator Maxwell Edgar Hargreaves
Date range June 1944    Quantity 1 file
Inventory Identifier 6-13 Series 6

Published by the Australian Science and Technology Heritage Centre on AustehcWeb, April 2004
With support from Ian Potter Foundation, CRA Ltd and The University of Melbourne
Listed by Gavan McCarthy
HTML edition Ailie Smith
Updated 8 November 2007
http://www.austehc.unimelb.edu.au/guides/harg/HARGS006.htm

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