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Low-speed experimental determination of the effects of leading-edge radius and profile thickness on static and oscillatory lateral stability derivatives for a delta wing with 60 degrees of leading-edge sweep
Author:
Fletcher, Herman S
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4341
Link:
https://digital.library.unt.edu/ark:/67531/metadc57408/
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