NASA NTRS · 19870000333
Aluminum Alloys for High Temperatures
Abstract
New Al/Li alloys processed by rapid solidification show greatly improved strength-to-density ratios. Alloys suitable substitutes for heavier titanium alloys and weaker aluminum alloys in high-performance aircraft, bombers, and transports. Also suitable for use in high-performance-aircraft structures heated by engines and normally constructed from titanium alloys.
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Meschter, Peter J., Lederich, Richard J., O'Neal, James E.. 1987-07-01. Aluminum Alloys for High Temperatures. https://ntrs.nasa.gov/citations/19870000333
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