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 29
28 NACA RM L9E24 … 0 ch T 004 n8 -.008 .002 Cis .00/ 0 O 4 8 12 16 20 cCjdeg Figure 9.- The effects of high-lift and stall-control devices on the aileron hinge-moment and effectiveness parameters C^, ch5^ and Cj5.
NASA Technical Reports Server (NTRS)
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