Flight Investigation of Lateral Control Devices for Use with Full-Span Flaps (1936)
NASA Technical Reports Server (NTRS) · leaf 7
4 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS Figure 3.—Fairchild 22 airplane. 197" Areas: sq. ft. sg.ft Areas: file va tor Wing 172 10.4 Rudder Aileron 29 6 Stabilizer 15.8 Fin 4.1 _J_ PlQUEl 5. -Lay-out of standard Fairchild 22 wing and aileron installation Weight, 1500 lb Horsepower 95 .7… … Time from initial movement of control column, seconds Figure 4.—Three-view drawing of the Fairchild 22 airplane. Figure 6 — Results of lag tests of various control devices on the Fairchild 22 airplane.
NASA Technical Reports Server (NTRS)
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