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Through-Width and Through-Thickness Edge Effects on Tensile Properties of Thick AA2219 PlateDuring the latter stages of the investigation into AA 2219 low, short transverse tensile ductility related to copper rich theta particles (Al2Cu), the NASA Engineering and Safety Center (NESC) team discovered an “edge effect,” where improved ductility and strength was observed in tensile specimens obtained from material close to the plate’s edges in the width direction. Therefore, an in-depth metallurgical investigation was carried out to determine the root causes of the edge effect. The investigation revealed a through-width edge effect and a through-thickness edge effect. With respect to mechanical properties, the edge effects manifested as variations in ductility and strength with respect to through-width and through-thickness locations. Thermo-mechanical processing of the material, specifically, rolling temperature, rolling strain, and quench rates, and their effects on microstructural evolution of theta particles are identified as root causes of the width and thickness edge effects. Additionally, differential scanning calorimetry was identified as an efficient and effective screening method for determining through-thickness areas of high Al-Cu eutectic phases which are associated with high concentrations of theta particles related to low ductility and strength.
Document ID
20240000329
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
P S Chen
(Jacobs ESSCA Group Huntsville, Alabama)
W M Medders
(Marshall Space Flight Center Redstone Arsenal, United States)
C H Su
(Marshall Space Flight Center Redstone Arsenal, United States)
W G Tilson
(Marshall Space Flight Center Redstone Arsenal, United States)
D N Wells
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
January 9, 2024
Publication Date
March 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Metals and Metallic Materials
Report/Patent Number
NASA/TM-20240000329
NESC-RP-21-01721
Funding Number(s)
WBS: 869021.01.23.01.01
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Short-Transverse Properties
Tensile Properties
Aluminum Alloy 2219
NASA Engineering and Safety Center
Theta Particles
Differential Scanning Calorimetry
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