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Control surface flutter can be avoided by: 1. a high stiffness of the structure...
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Control surface flutter can be avoided by: 1. a high stiffness of the structure to which the control surface is attached. 2. a low stiffness of the structure to which the control surface is attached. 3. locating a balancing mass in front of the control surface hinge line. 4. locating a balancing mass behind the control surface hinge line. The combination that regroups all of the correct statements is:
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