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.
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.
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