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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