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Experimental Investigation of Oscillatory Aerodynamic Forces, Moments and Pressures Acting on a Tapered Wing Oscillating in Pitch at Mach Numbers from 0.40 to 1.07
Results of Initial Wind-tunnel Flutter Experiments at Low Speed with a Towed Airplane Model Having a 40 Degree Sweptback Wing of Aspect Ratio 3.62 Equipped with Pylon-mounted Stores
Aerodynamic damping and oscillatory stability of a model of a proposed HL-10 vehicle in pitch at Mach numbers from 0.20 to 2.86 and in YAW at Mach numbers from 0.20 to 1.20