Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices (1949)
NASA Technical Reports Server (NTRS) · leaf 15
NACA RM L9E2^ Ik Ffap joins upper surface approximately i/2 inch behind wing leading edge 4.0 radius 0.5 diameter Section A-A (enlarged) Section B-B (enlarged) … Figure 2.- Details of wing highr-lift and stall-control devices.
NASA Technical Reports Server (NTRS)
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