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An Automatically Variable Control Linkage and Its Effect on the Lateral-control Characteristics of a High-speed Fighter Airplane

出版	National Advisory Committee for Aeronautics, 1944
URL	http://books.google.com.hk/books?id=2Jkn5GOR01IC&hl=&source=gbs_api

註釋Summary: An analysis and a preliminary design were made for a control linkage that varies automatically with dynamic pressure. This device can provide greater lateral control than a fixed control linkage at all but one airspeed without additional aerodynamic balance. The mechanical construction should present no unusual problems and both the weight and volume of the device appear sufficiently small for use in single-seat fighter airplanes as well as in large machines.