Research and Development of Aircraft Control Actuation Systems. The Development of a Flight Control System Simulator, Research on a Control Surface Flutter Suppression Technique and High Temperature Testing of Mil-H-83282.
Final rept. Jan 74-Feb 75,
DYNAMIC CONTROLS INC DAYTON OHIO
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This report presents the results of the following three research and development activities the design, fabrication and test of a multi-channel flight control system hybrid simulator the analysis and application of a flutter damping technique for hydraulically actuated slab type control surfaces and the experimental testing of Mil-H-83282 hydraulic fluid in a pumping system at elevated temperature.