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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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张新宇 [3]
仲峰泉 [1]
卢洪波 [1]
孙文明 [1]
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航空学报 [3]
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Source Publication：航空学报
Creator：zhangxinyu分张新宇
Community：高温气体动力学国家重点实验室
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微波增强滑移电弧等离子体辅助超声速燃烧
期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors:
孟宇
;
顾洪斌
;
孙文明
;
张新宇
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View/Download：246/34
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Submit date：2019/12/16
超燃冲压发动机
超声速燃烧
等离子体助燃
滑移电弧
微波
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
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Adobe PDF(711Kb)
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View/Download：337/81
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Submit date：2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流
矩形横截面螺旋管湍流流动与传热特性的数值研究
期刊论文
航空学报, 2013, 卷号: 34, 期号: 6, 页码: 1269-1276
Authors:
邢云绯
;
仲峰泉
;
张新宇
Adobe PDF(894Kb)
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View/Download：971/319
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Submit date：2013/07/10
螺旋管
湍流
曲率
传热
矩形
