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 14
NACA RM L52B15a CONFIDENTIAL 13 … Figure 5.- Variation of Reynolds number with Mach number. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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