Effect of Horizontal-Tail Location on Low-Speed Static Longitudinal Stability and Damping in Pitch of Model Having 45° Sweptback Wing and Tail Surfaces.
Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of model having 45° sweptback wing and tail surfaces
NACA -- Tech Note
1951
26 pages
Illus, Diagrs, Charts, Tables
Report
English
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