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 21
20 NACA RM L9E24 … Figure 5.- Aileron characteristics of wing with leading— and trailing-edge flaps deflected.
NASA Technical Reports Server (NTRS)
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