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NACA-TN-3462

Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:31:54Z
date available2017-09-04T15:31:54Z
date copyright07/01/1955
date issued1955
identifier otherOEYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/33448
description abstractResults are presented of tests to determine the effect of heating at uniform temperature rates from 0.2 degrees to 100 degrees F. per second on the tensile properties of 7075-T6 d(75s-T6) and 2024-T3 (24s-T3) aluminum-alloy sheet under constant-load conditions. Yield and rupture stresses, obtained under rapid-heating conditions, are compared with results of elevated-temperature stress-strain tests for 1/2-hour exposure. Master yield-and-rupture-stress curves based on linear temperature-rate parameter are presented. Yield and rupture stresses and temperatures may be predicted by means of master curves and the parameter.
languageEnglish
titleNACA-TN-3462num
titleTensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant loaden
typestandard
page48
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
subject keywordsAIRCRAFT STRUCTURES
subject keywordsALUMINUM ALLOYS
subject keywordsCONSTRUCTION MATERIALS
subject keywordsCREEP STRENGTH
subject keywordsFRACTURE STRENGTH
subject keywordsMISSILE STRUCTURES
subject keywordsRATES (PER TIME)
subject keywordsSTRAIN RATE
subject keywordsSTRESS-STRAIN RELATIONSHIPS
subject keywordsTEMPERATURE
subject keywordsTENSILE PROPERTIES
subject keywordsTENSILE TESTS
subject keywordsTHERMODYNAMIC PROPERTIES
subject keywordsYIELD STRENGTH


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