AVIATION TECHNOLOGICAL INSTITUTE, MOSCOW, VOL 51, 1961: COLLECTION OF ARTICLES,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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Contents Mechanical properties of aluminum alloys D16 and V95 in connection with the technology of manufacturing semi-finished products from them Fatigue properties of aluminum alloy used for helicopter blades Influence of concentration of stresses on fatigue of aluminum alloy V95 Effect of concentration of stresses on static crack strength of aluminum alloy V95 Method of determining stress-rupture strength of slightly embrittled materials Investigation of mechanical properties of aluminum alloys during compression.
- Metallurgy and Metallography