首页>
美国政府科技报告
>Experimental static aerodynamic forces and moments at low speed on a missile model during simulated launching from the 25-percent-semispan and wing-tip location of a 45 degree sweptback wing-fuselage combination
【24h】
Experimental static aerodynamic forces and moments at low speed on a missile model during simulated launching from the 25-percent-semispan and wing-tip location of a 45 degree sweptback wing-fuselage combination