Influence of Wing and Fuselage on Vertical-Tail Contribution to Low-Speed Rolling Derivatives of Midwing Airplane Models with 45° Sweptback Surfaces.
Influence of wing and fuselage on vertical-tail contribution to low-speed rolling derivatives of midwing airplane models with 45° sweptback surfaces
NACA -- Tech Note
1951
55 pages
Diagrs, Charts, Tables
Report
Englisch
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Engineering Index Backfile | 1943
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