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 22
21 NACA RM L52B15a CONFIDENTIAL O Wing-tip control n0 end plflte □ Wing-tip control with end plate O Flap-type control (unpublished data) … Figure 12.- The variation of pitching-moment coefficient with control deflection for normal-force coefficient of 0.1 at various Mach numbers. Results from fin-off flap-type configuration presented for comparison.
NASA Technical Reports Server (NTRS)
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