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Preliminary Investigation of the Compressive Strength and Creep Lifetime of 2024-T3 (formerly 24S-T3) Aluminum-alloy Plates at Elevated Temperatures

出版	National Advisory Committee for Aeronautics, 1955
URL	http://books.google.com.hk/books?id=EJ8lq2OL8RQC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋The results of elevated-temperature compressive strength and creep tests of 2024-T3 (formerly 24S-T3) aluminum-alloy plates supported in V-grooves are presented. For determining elevated-temperature strength, where creep effects are negligible, a relation previously developed for predicting plate compressive strength at room temperature was satisfactory. Creep-lifetime results are presented for the plates in the form of master creep-lifetime curves by using a time-temperature parameter that is convenient for summarizing tensile creep-rupture data. A comparison is made between tensile and compressive creep lifetime for the plates, and the magnitude by which the design stress is decreased because of material creep and loss of strength due to exposure at elevated temperatures is indicated.