Application and control of continuously varying loading which simulate flight loading, producing fatigue damage encountered by aircraft structure can be accomplished electro-hydraulically with results comparable to actual airplane service experience; force feedback electrohydraulic servo system consists of load programmer, controller, load cell, electro-servo valve with hydraulic manifold, hydraulic actuator, and load recording equipment.
Test methods and equipment -- Model KC-135 airplane wing fatigue test
Experimental Mechanics
Experimental Mechanics ; 3 , n 7
1963
5 pages
Aufsatz (Zeitschrift)
Englisch
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