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The paper brought to light a previous result of the author, used in the design of hydraulic servos actuating flight controls of the airplanes IAR 93 and IAR 99. The results highlights the importance of the the kinematics of the rigid feedback linkage of the hydraulic servo in an aeroservoelastic frame.

The kinematics of the rigid feedback linkage, the impedance of the hydraulic servomechanism and the flutter occurrence