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Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy
Author:
Heimerl, George J.
Year:
1945
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-32, NACA-ARR-L5F08b
Link:
https://digital.library.unt.edu/ark:/67531/metadc64990/
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