Effect of unswept wing on contribution of unswept-tail configurations to low-speed static -- And rolling-stability derivatives of midwing airplane model.
Effect of unswept wing on contribution of unswept-tail configurations to low-speed static -- And rolling-stability derivatives of midwing airplane model
Nat Advisory Committee Aeronautics -- Tech Note
1950
47 pages
Illustrations, Diagrams, Charts
Report
English
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