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基于舰载机起降限制的舰船气流场特性评估方法初探
引用本文:陆超,姜治芳,王涛.基于舰载机起降限制的舰船气流场特性评估方法初探[J].中国舰船研究,2010,5(1):39-42.
作者姓名:陆超  姜治芳  王涛
作者单位:中国舰船研究设计中心,湖北,武汉,430064
摘    要:对具有搭载舰载机能力的舰船而言,其气流场特性的评估取决于对相应舰载机的起降气流条件限制。通过对美国LHA型舰缩比模型的数值建模,结合两种舰载机起降的气流场限制条件对计算结果进行对比分析。在相同定常来流工况下,分别以±15°风向角对该型舰数值模型的两个起降点进行模拟取值,结合直升机和固定翼短距/垂直起落飞机的起降特性和气流限制条件,尝试提出一种评估舰船气流场特性的直观方法,并得出不同甲板气流区域受上层建筑影响的有关结论。

关 键 词:空气流场特性  风向角  航速  舰载机  起飞/降落

Simplified Evaluation of Ship Airwake Characteristics for Takeoff/Landing of Shipborne Aircraft
Lu Chao Jiang Zhi-fang Wang Tao China Ship Development , Design Center,China.Simplified Evaluation of Ship Airwake Characteristics for Takeoff/Landing of Shipborne Aircraft[J].Chinese Journal of Ship Research,2010,5(1):39-42.
Authors:Lu Chao Jiang Zhi-fang Wang Tao China Ship Development  Design Center    China
Institution:Lu Chao Jiang Zhi-fang Wang Tao China Ship Development , Design Center,430064,China
Abstract:An evaluation of the airwake for aircraft takeoff/landing has its limitation on the conditions of ship. This paper described the adoption of LHA scaled model, takeoff/landing of aircrafts and their limitation of airwake etc. Under the same steady flow condition, by simulating the two takeoff/landing points of the scaled model with -+15~ wind angles, and combining their takeoff/landing characteristics and airwake limitations of helicopters and STOVL aircrafts, it carried out a simplified evaluation of ship airwake characteristics. Conclusions show that different deck airwake areas are effected by the superstructure.
Keywords:airwake characteristics  wind angle  speed  shipborne aircraft  takeoff / landing  
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