Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions /

Results are presented of rapid-heating tests to deternine the tensile strength of lnconel and RS-120 titanium-alloy sheet heated to failure at uniform temperature rates from 0.2 F to 100 degrees F per second under constant load condltions. Yield and rupture stresses, obtained by rapid heating, are c...

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Bibliographic Details
Main Author: Heimerl, George J
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Inge, John E, Kurg, Ivo M
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1956]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3731
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Stanford University

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Call Number: NACA TN 3731