Wind tunnel research comparing lateral control devices, particularly at high angles of attack XI : various floating tip ailerons on both rectangular and tapered wings
This is a 1933 NACA technical report from the NASA Technical Reports Server, a wind tunnel study of lateral control devices, specifically floating tip ailerons on rectangular and tapered wings, written for aeronautical engineers. Its pictures are plain engineering graphs of rolling-moment coefficient against aileron deflection, with grid lines and labelled curves, plus one wing layout drawing with dimensions, offering a designer little beyond the stark plotted-line vocabulary of mid-century technical charts.
