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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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