Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61

Author: Letko, William
Year: 1948
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1671
Link: https://digital.library.unt.edu/ark:/67531/metadc54716/

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