Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IV : floating tip ailerons on rectangular wings (1933)
NASA Technical Reports Server (NTRS) · leaf 2
ling moment due to the asymmetric the ailerons. The floating angles of the left aileron distribution of the load along the span when the wing with respect to the chord of the model, designated 5^, is rolling. The results of the free-autorotation tests are also included in these tables. are given in… … Figure 1.—Diagrams of the various model arrangements with floating tip ailerons above are with respect to the wind axis, which corre- were made at 0° yaw, in which the model was mounted sponds to the center line of the air stream. on the spindle, which was free to rotate. In these tests the range…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
