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Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 0-1HTA Magnesium Alloy
Author:
Heimerl, George J.
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1156
Link:
https://digital.library.unt.edu/ark:/67531/metadc55074/
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