Effects of Modifications to a Control Surface on a 6-Percent-Thick Unswept Wing on the Transonic Control-Surface Flutter Derivatives
1958
69 pages
Report
No indication
English
Aerodynamics , Control surface , Flutter analysis , Pressure measurement , Transonic flutter , Unswept wing , Aerodynamic , Analysis , Cell , Chord , Control , Damping , Derivative , Dynamic , Elevator , Flap , Flutter , Hinge , Measurement , Moment , Pressure , Shock , Surface , Transonic , Triangle , Unswept , Vibration , Wave , Wedge , Wing