1. 上海交通大学 机械与动力工程学院， 上海 200240； 2. 中国商飞民用飞机试飞中心， 上海 200232； 3. 中国商飞上海飞机客户服务有限公司， 上海 200240
收稿日期:2017-04-06通讯作者:董威，男，教授，博士生导师，电话（Tel.）:021-34204410；E-mail:Wdong@sjtu.edu.cn.作者简介:赵彬彬（1988-），女，江苏省苏州市人，硕士生，主要研究方向为电加热防除冰和等离子体主动流动控制.基金资助:国家自然科学基金资助项目（11572195），国家重点基础研究发展规划（973）项目（2015CB755800），航空工业产学研专项(cxy2013SHJD27)Experimental Study on the Anti-Icing Performance of Plasma Jet I. Parametric Analysis of DBD-PA and Verification on the Anti-Icing Performance
ZHAO Binbin,DONG Wei,LIU Juan,ZHANG Yi1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China; 2. CFTC, Commercial Aircraft Corporation of China, Ltd., Shanghai 200232, China; 3. SACSC, Commercial Aircraft Corporation of China, Ltd., Shanghai 200240, China
Received:2017-04-06摘要/Abstract
摘要： 在冰风洞中开展了结冰条件下NACA0012机翼模型的等离子体射流防冰性能实验研究.设计加工了等离子体射流激励器并粘接于机翼表面，热电偶巧妙埋设于激励器下方以检测防冰效果.实验验证了激励器掩埋电极上方等离子体射流的防冰性能,考察了防冰性能随激励电压和激励频率等参数变化的规律.
关键词: 防冰性能, 等离子体射流, 冰风洞, 介质阻挡放电, 激励器
Abstract: The anti-icing performance of plasma jet fixed on NACA0012 wing model is studied in icing wind tunnel. A plasma jet actuator is designed and installed on the wing model surface, and thermocouples are cleverly embedded beneath the actuator to detect the anti-icing effect. A parametric analysis is performed to investigate the relationship of the anti-icing performance with voltage and frequency, respectively, and the anti-icing effect of plasma jet above insulated electrode is verified.
Key words: anti-icing performance, plasma jet, icing wind tunnel, dielectric-barrier-discharge, actuator
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