Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model

Author: Letko, William
Year: 1950
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2175
Link: https://digital.library.unt.edu/ark:/67531/metadc55522/

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