【摘要】 为探索高空远程滑翔UUV空气动力学基本特性,针对高空远程滑翔UUV详细设计了风洞试验模型,并通过试验分析了攻角和导流罩对高空远程滑翔UUV亚音速滑翔时升阻特性的影响,得到了高空远程滑翔UUV升阻特性的基本规律,为高空远程滑翔UUV总体、气动的进一步设计提供了依据。更多还原

【Abstract】 In order to explore the basic aerodynamic characteristics of high-altitude long-rang glider UUV,the wind tunnel test model is designed for a highaltitude long-rang glider UUV.Further more,the lift-drag characteristics affected by the angle of attack and the cover of the diversion when the high-altitude long-rang glider UUV is gliding under the condition of subsonic speed are analyzed,and the basic rules of lift-drag characteristics are acquired.The results of experiment can guide the conceptual design and aerodynamic design of the high-altitude long-rang glider UUV.更多还原