ONE of the primary considerations in the design of high performance aircraft is the attainment of a high power/weight ratio for the unloaded machine, while at the same time ensuring complete reliability under the most exacting service conditions.
Gadd, E.R. (1935), "Magnesium Alloys in Aeroplanes: The Properties, Methods of Treatment and Uses of an Interesting Material", Aircraft Engineering and Aerospace Technology, Vol. 7 No. 12, pp. 299-302. https://doi.org/10.1108/eb029994Download as .RIS
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