Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials
Description:
Experimental data are presented on the variation of the modulus of rigidity in the temperature range -20 to +50 degrees C. of a number of metals which are of possible use for elastic elements for aircraft and other instruments. The methods of the torsional pendulum was used to determine the modulus of rigidity and its temperature coefficient for aluminum, duralumin, monel metal, brass, phosphor bronze, coin silver, nickel silver, three high carbon steels, and three alloy steels. It was observed…
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Date:
March 7, 1930
Creator:
Brombacher, W. G. & Melton, E. R.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department