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Fatigue Life of Flow-Formed Aluminum 2195 and 6061 AlloysThe successful design and fabrication of metallic cryotanks for commercial aviation applications require lightweight, durable materials capable of withstanding high pressures and cryogenic temperatures through tens of thousands of thermomechanical refueling cycles. Flow forming is an advanced manufacturing technique that offers high-rate production and scalability for fabricating integrally stiffened cylinders suitable for cryotank applications. This work establishes the durability of flow-formed aluminum alloys by characterizing their fatigue life performance under conditions that mimic cryotank refueling cycles. Residual stresses in flow-formed aluminum-lithium (Al-Li) 2195-T6 cylinders were assessed using the contour method and found to be minimal. Fatigue life testing was conducted on flow-formed Al-Li 2195-T6 at room temperature and cryogenic temperatures (-321°F [-196°C]), with wrought Al-Li 2195-T6 serving as a baseline for comparison. Results showed that flow-formed materials exhibited fatigue performance comparable to or better than wrought materials, with no statistically significant differences observed between different specimen orientations relative to processing directions. Fractography revealed reduced delaminations in the flow-formed Al-Li 2195 samples as compared to wrought, indicating potential improvement to the microstructure that could result in improved service properties. Texture analysis using electron backscattered diffraction (EBSD) indicated recrystallization during heat treatment, potentially contributing to reduced delamination susceptibility. These findings demonstrating flow-formed material durability coupled with the high manufacturing efficiency of flow forming, makes flow forming an attractive process to produce aircraft cryotanks.
Document ID
20260001601
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Andrew Boddorff
(Langley Research Center Hampton, United States)
John Newman
(Langley Research Center Hampton, United States)
Wesley Tayon
(Langley Research Center Hampton, United States)
Elizabeth Urig
(Analytical Mechanics Associates (United States) Hampton, United States)
Date Acquired
February 20, 2026
Publication Date
March 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Metals and Metallic Materials
Mechanical Engineering
Report/Patent Number
NASA/TP-20260001601
Funding Number(s)
WBS: 109492.02.07.09.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
EBF3
Additive Manufacturing
Automated Inspection Detection and Repair
Laser-wire DED
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