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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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