Aircraft Stability Analysis Including Unsteady Aerodynamic Effects
Aircraft Stability Analysis Including Unsteady Aerodynamic Effects
Aircraft Stability Analysis Including Unsteady Aerodynamic Effects
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890.060.04θ = 20 degModel responseExperimental data0.02C l0-0.02-0.04-0.060 0.2 0.4 0.6 0.8 1time, sFigure 3-11 Rolling moment coefficient time-history at θ 0 = 20 deg, secondinvestigated model.