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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