Present Status of Lateral-Control Devices for use with Split Flaps, Special Report (1933)
NASA Technical Reports Server (NTRS) · leaf 8
yawing moments. The rolling-^moment coefficient increases in magnitude as tiie aiigle of attack is increased up to and tb^rougli the stall (these ailerons are similar tt ifiJtltrs in this respect), and fair values are maintained to very high angles of attack. This location has also "been foxtnd … promising in an investigation carried on during approxi- mately the same period as the H.A.C.A. tests at California Institute of Technology, in cooperation with the Douglas and Northrop companies (reference 2)• Plight tests have been made on external ailerons in approximately this same location…
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