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
This is a 1949 NASA technical report, issued by NASA's Technical Reports Server, presenting low-speed wind-tunnel test results on aileron control for a wing with 42-degree swept leading edge, with and without high-lift devices, for aeronautical engineers. The pictures are line graphs of coefficients plotted against angle of attack and aileron deflection, with symbol-coded data series, grid backgrounds and small NACA labels. A designer may find in them only a sparse, technical vocabulary of plotted curves, useful as abstract line-and-marker patterns.
