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岳连捷 [1]
李虹杨 [1]
杨慧 [1]
路文睿 [1]
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北京航空航天大学学报 [1]
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Indexed By:CSCD
Date Issued:2018
Funding Organization:为研究高超声速进气道的性能参数随飞行高度、来流湍流度及来流马赫数的变化规律,并考察其压缩面上的边界层转捩现象对进气道性能的影响,采用本课题组程序平台HGFS所发展的γ-Re_θ转捩模型进行了一系列的数值模拟工作,并对相应的流动现象和机理进行分析.首先,利用进气道压缩面的简化模型对γ-Re_θ转捩模型经验关联公式的高超声速改进方法进行了验证
Community:高温气体动力学国家重点实验室
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基于工程转捩模型的高超声速进气道特性
期刊论文
北京航空航天大学学报, 2018, 卷号: 44, 期号: 7, 页码: 1408-1418
Authors:
杨慧
;
路文睿
;
李虹杨
;
岳连捷
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Submit date:2018/10/24
高超声速进气道
转捩模型
飞行高度
湍流度
数值模拟