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.
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
1975
202 pages
Report
Keine Angabe
Englisch
British Library Conference Proceedings | 2011
|Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft
SAE Technical Papers | 1987
|