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高温环境辅助进气合成射流的激励器性能

洪亮 额日其太 宫建

洪亮, 额日其太, 宫建. 高温环境辅助进气合成射流的激励器性能[J]. 航空动力学报, 2020, 35(1): 126-134. doi: 10.13224/j.cnki.jasp.2020.01.015
引用本文: 洪亮, 额日其太, 宫建. 高温环境辅助进气合成射流的激励器性能[J]. 航空动力学报, 2020, 35(1): 126-134. doi: 10.13224/j.cnki.jasp.2020.01.015
HONG Liang, Eriqitai, GONG Jian. Performace of novel synthetic jet actuator under high ambient temperature[J]. Journal of Aerospace Power, 2020, 35(1): 126-134. doi: 10.13224/j.cnki.jasp.2020.01.015
Citation: HONG Liang, Eriqitai, GONG Jian. Performace of novel synthetic jet actuator under high ambient temperature[J]. Journal of Aerospace Power, 2020, 35(1): 126-134. doi: 10.13224/j.cnki.jasp.2020.01.015

高温环境辅助进气合成射流的激励器性能

doi: 10.13224/j.cnki.jasp.2020.01.015
基金项目: 国家自然科学基金(11572027)

Performace of novel synthetic jet actuator under high ambient temperature

  • 摘要: 对高温环境下活塞式合成射流激励器的流场进行了数值模拟和试验研究,对比了激励器工作频率和射流孔直径,对常规、辅助进气激励器性能的影响。结果表明:在高温环境下,相对于常规进气,辅助进气可以显著地提高激励器性能,激励器吸气量、腔体峰值压比和射流峰值动量提高的同时,激励器出口截面射流峰值速度略有下降。辅助进气装置的效能最大区域为高工作频率或者小射流孔直径。相对于常规激励器,辅助进气激励器的吸气量、腔体峰值压比和射流峰值动量的增加幅度最大,分别增加了常规激励器的23073%、10397%和10737%(工作频率为250 Hz,射流孔直径为2 mm)。

     

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出版历程
  • 收稿日期:  2019-09-10
  • 刊出日期:  2020-01-28

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