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美国政府科技报告
>Experimental static aerodynamic forces and moments at high subsonic speeds on a canard missile during simulated launching from the midsemispan location of a 45 degree wing-fuselage-pylon combination at zero sideslip
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Experimental static aerodynamic forces and moments at high subsonic speeds on a canard missile during simulated launching from the midsemispan location of a 45 degree wing-fuselage-pylon combination at zero sideslip