Comparison of 24S-T aluminum alloy flat compression panels having longitudinal Z-section stiffeners and, panels having flat FS-1H magnesium alloy sheet and longitudinal 24S-T aluminum alloy Z-section stiffeners.
Compressive-strength comparisons of panels having aluminum-alloy sheet and stiffeners with panels having magnesium-alloy sheet and aluminum-alloy stiffeners
Nat Advisory Committee Aeronautics Tech Note
1947
24 pages
12 Supp Sheets
Report
English
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