Accession Number : AD0010717


Title :   COMBINED-STRESS FATIGUE STRENGTH OF 76S-T61 ALUMINUM ALLOY WITH SUPERIMPOSED MEAN STRESSES AND CORRECTIONS FOR YIELDING


Descriptive Note : Technical note


Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC


Personal Author(s) : FINDLEY, WILLIAM N


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/010717.pdf


Report Date : May 1953


Pagination or Media Count : 100


Descriptors :   *ALUMINUM ALLOYS , *FATIGUE(MECHANICS) , TEST EQUIPMENT


Subject Categories : Metallurgy and Metallography
      Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE