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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 28

An illustration from 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, leaf 28 — NACA RM L9E24 27 … Figure 8.— The variation of rolling-moment characteristics with aileron deflection for various model configurations.

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