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固定翼飞机截面绕流结构着水冲击载荷特性研究

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针对水上飞机常用的V型和陆基飞机常用的圆柱绕流结构,开展了模型着水载荷试验,对比分析了两种不同截面绕流结构的载荷特性。研究结果表明:V型绕流结构具有较好的载荷特性,在着水过程中压力峰值变化周期较长、峰值相对较小,峰值作用半周期在 0。1s左右,压力位置、速度对峰值影响明显,越靠近对称面位置,着水速度越大压力峰值越大。圆柱形绕流结构具有压力峰值大、作用周期短的特点,同等条件下对称面位置的压力峰值是V型绕流结构最大压力的 8。7 倍,峰值作用半周期仅在0。5ms左右。
Study on water shock load characteristics of fixed-wing aircraft cross-sectional flow structure
Aiming at the V-shaped and cylindrical winding structures commonly used in land-based air-craft,the model water load test was carried out,and the load characteristics of two different cross-sectional flow winding structures were compared and analyzed.The results show that the V-shaped flow around structure has good load characteristics,the pressure peak change period is long and the peak value is rela-tively small during the watering process,the half cycle of the peak is all in 0.1 s,the pressure position and velocity have obvious effects on the peak,which is close to the symmetrical plane position,and the larger the landing speed,the greater the pressure peak.The cylindrical flow around structure has the characteris-tics of large pressure peak and short action cycle,and the pressure peak at the symmetrical surface position under the same conditions is 8.7 times the maximum pressure of the V-shaped flow structure,and the half cycle is only about 0.5 ms.

fixed-wing aircraftstructure sectionditchingwater loadmodel test

黄淼、吴彬、汪小翔

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中国特种飞行器研究所,448035 荆门

固定翼飞机 截面绕流结构 着水 冲击载荷 试验研究

2024

应用力学学报
西安交通大学

应用力学学报

CSTPCD北大核心
影响因子:0.398
ISSN:1000-4939
年,卷(期):2024.41(6)