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Aerodynamic Characteristics of Gun-Launched Loitering Munitions and Its Shape Design
Author(s): 
Pages: 953-956,961
Year: Issue:  11
Journal: Transactions of Beijing Institute of Technology

Keyword:  管式发射巡飞弹空气动力学气动设计折叠翼充气翼;
Abstract: 讨论了管式发射巡飞弹的气动特点和设计,分析了折叠翼的低雷诺数高升力翼型的气动特性、设计方法以及弹翼的折叠设计,并分析了柔性充气翼的发展、优缺点、气动特性以及目前存在的技术难题.研究结果表明,封装后的充气翼不会破坏机翼结构的整体性,体积降为展开体积的1/10,避开了传统飞行器复杂的折叠结构,质量也大为减轻.分析结果表明充气翼的发展优势以及巡飞弹气动一体化总体设计技术的重要性.
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