护卫舰排气扩散的流场可视化与分析研究

IF 0.5 Q4 TRANSPORTATION
E. Dobrucalı
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引用次数: 0

摘要

通过风洞流动可视化试验,分析了射流速度和偏航角对某型护卫舰排烟散度的影响。还进行了分析研究,以获得排气羽流轨迹。1/100比例的通用护卫舰,在舰尾有一个直升机平台,在实验研究期间建造和使用。考虑了护卫舰的前进和后退巡航。羽流高度和排气动量随速度比的增大而增大。对于K=0.2等低速比率,观察到烟雾滋扰问题。当偏航角大于10°时,羽流也指向直升机平台。实验结果与三种不同速度比下的解析解进行了比较。实验结果与分析结果的符合性是一致的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Flow visualization and analytical study on the exhaust gas diffusion of a frigate
Wind tunnel flow visualization tests were conducted to analyse the efflux velocity impacts and the yaw angle on the smoke dispersion of the exhaust for a generic frigate. An analytical study was also implemented to obtain the exhaust plume trajectories. The 1/100 scale generic frigate, having a platform for helicopters on the aft of the ship, was built and employed during the experimental study. The forward and astern cruises of the frigate were considered. It is found that the plume height and the exhaust gases momentum increase with the velocity ratio. The problem of smoke nuisance was observed for the ratios with low velocity such as K=0.2. The plume was also directed towards the helicopter platform when the yaw angles are higher than 10°. The experimental results are compared with the analytical solutions for three different velocity ratios. The compliance between the experimental and analytical results is found to be consistent.
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来源期刊
CiteScore
1.50
自引率
0.00%
发文量
19
审稿时长
8 weeks
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