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 10
9 CONFIDENTIAL NACA RM L52B15a Figure 1.- Model and vane on wing of airplane. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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