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Effect of a finite trailing-edge thickness on the drag of rectangular and delta wings at supersonic speeds
Author:
Klunker, E. B.
Year:
1952
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2828
Link:
https://digital.library.unt.edu/ark:/67531/metadc56365/
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