A Method of Selecting the Thickness, Hollowness, and Size of a Supersonic Wing for Least Drag and Sufficient Bending Strength at Specified Flight Conditions

Author: Amick, James L.
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2754
Link: https://digital.library.unt.edu/ark:/67531/metadc56403/

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