Flutter.

29. Flutter. For Multiengine turbopropeller powered airplanes, a dynamic evaluation must be made and must include -
(a) The significant elastic, inertia, and aerodynamic forces associated with the rotations and displacements of the plane of the propeller; and
(b) Engine-propeller-nacelle stiffness and damping variations appropriate to the particular configuration.

Source

14 CFR § Special_Federal_Aviation_Regulation_No._23


Scoping language

None
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