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固定翼二维弹道修正引信升力翼面位置的影响 被引量:2
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作者 李曼 张英 +2 位作者 霍鹏飞 施坤林 石晓峰 《探测与控制学报》 CSCD 北大核心 2018年第3期31-35,共5页
固定翼二维弹道修正引信研究需要了解翼面之间的气动干扰。鉴于查不到相关文献,采用流场计算中广泛使用的数值模拟方法,计算引信及翼面的气动参数和修正弹的流场分布。计算结果表明,在固定翼二维弹道修正引信翼面尺寸和安装角度不变的... 固定翼二维弹道修正引信研究需要了解翼面之间的气动干扰。鉴于查不到相关文献,采用流场计算中广泛使用的数值模拟方法,计算引信及翼面的气动参数和修正弹的流场分布。计算结果表明,在固定翼二维弹道修正引信翼面尺寸和安装角度不变的前提下,随着升力翼面安装位置的前移,固定翼二维弹道修正引信的导转力矩、导转翼面的阻力和导转力矩以及升力翼面的阻力和升力均有所增加,而对导转翼面升力的影响较小;在跨音速时,引信及翼面的气动参数均变化较大。 展开更多
关键词 二维弹道修正引信 翼面气动干扰 数值模拟 气动特性
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An Experimental Study on Aerodynamic Sound Generated from Wake Interference of Circular Cylinder and Airfoil Vane in Tandem 被引量:1
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作者 MizueMUNEKATA KaoruKAWAHARA +2 位作者 TakamasaUDO HiroyukiYOSHIKAWA HidekiOHBA 《Journal of Thermal Science》 SCIE EI CAS CSCD 2006年第4期342-348,共7页
The purpose of this study is to investigate the characteristics of aerodynamic sound generated from wake interference of circular cylinder and airfoil vane located in tandem and to clarify the generation mechanism of ... The purpose of this study is to investigate the characteristics of aerodynamic sound generated from wake interference of circular cylinder and airfoil vane located in tandem and to clarify the generation mechanism of the sound source with discrete frequency. The effects of the interval between the cylinder and the airfoil on the characteristics of aerodynamic sound are investigated by acoustic measurement, flow visualization and exploration test of sound source. The relation between the flow field and the sound field with discrete frequency noise(DFN) is shown, and then it is found that the downstream airfoil works as the sound source of DFN, which has the frequency of vortex shedding from the upstream cylinder, when the interval of two bodies is longer than a critical distance. 展开更多
关键词 aerodynamic sound wake interference circular cylinder airfoil Karman's vortex flow visualization
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