Strainrange Partitioning Behavior of an Advance Gas Turbine Disk Alloy AF2-1DA

• 1 August 1980
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
• Vol. 17  (8) , 598-604
• https://doi.org/10.2514/3.57945

Abstract

Keywords

• STRESS ANALYSIS
• TENSILE STRENGTH
• COMPRESSIVE STRENGTH