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网格运动方式对水陆两栖飞机单船身阻力计算影响

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为提高水陆两栖飞机滑水阻力计算精度,基于黏性CFD计算软件STAR-CCM+,分别采用整体动网格法、常规动网格方法、重叠网格方法3 种不同的网格运动方式对单船身模型开展静水面滑行数值仿真,对比分析了网格运动方式对船底水气分布、兴波形状及阻力数值预报的影响特点,并与模型试验结果进行比较,验证不同方法的精度,结果表明,在排水航行和滑行状态下,3 种不同网格运动方式计算得到的阻力差异较小,且与试验值较为接近,而在过渡滑行阶段,不同网格运动方式计算得到的阻力值之间差异较大,其中,整体动网格法的计算结果与试验值误差较小,说明整体动网格法更适用于水陆两栖飞机单船身滑水阻力性能的计算.
Influence of Grid Motion Mode upon Numerical Calculation of Fuselage Resistance for an Amphibious Aircraft
In order to improve the accuracy of hydro-resistance prediction for an amphibious aircraft,the overall dynamic grid method,conventional dynamic grid method and overlapping grid method were adopted to conduct the numerical simulation by using viscous fluid dynamics software STAR-CCM+.The influences of different grid methods on the distribution of water vapor,the shape of wave generation and the numerical prediction of resistance were analyzed,and verification of different grid methods was made through the towing tank model test results.It was shown that under low speed navigation and high-speed taxiing condi-tions,the difference in resistance values calculated by the three different grid motion methods is relatively small and close to the experimental values,however,in transition phase of taxiing,difference in calculation values of the three grid motion modes is significant,and the calculation results of the overall dynamic grid method are in good agreement with the experimental values,in-dicating that the overall dynamic grid method is more reliable for the fuselage resistance calculation of amphibious aircraft.

fuselage of the amphibious aircraftnumerical simulationgrid motion moderesistancemodel test

高现娇、桑腾蛟、史圣哲

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中国特种飞行器研究所,湖北 荆门 448035

水陆两栖飞机单船身 数值模拟 网格运动方式 阻力性能 模型试验

工信部民用飞机专项

MJZ5-3N21-5

2024

船海工程
武汉造船工程学会

船海工程

CSTPCD北大核心
影响因子:0.361
ISSN:1671-7953
年,卷(期):2024.53(3)
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