Accession Number:

AD0648887

Title:

AVIATION TECHNOLOGICAL INSTITUTE, MOSCOW, VOL 51, 1961: COLLECTION OF ARTICLES,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1967-02-13

Pagination or Media Count:

82.0

Abstract:

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.

Subject Categories:

  • Helicopters
  • Metallurgy and Metallography
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE