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 18
NACA RM L52B15a CONFIDENTIAL 17 No end plate End plate on tip control surface … (c) M = 0.890. (d) M = O.933. Figure 10.- The variation of pitching-moment coefficient with normal- force coefficient for several control deflections with and without end plates at various Mach numbers. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
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