An Investigation of Longitudinal Control Characteristics of a Wing-tip Control Surface on a Sweptback Wing at Transonic Speeds by the NACA Wing-flow Method (1952)
NASA Technical Reports Server (NTRS) · leaf 12
-4^.- —« 11 CONFIDENTIAL NACA RM L52B15a … Figure 3-- Model with end plate on root of wing-tip control surface. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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