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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:EI
Creator:李虹杨
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Language:中文
Funding Organization:其次,以某型等熵压缩面的高超声速进气道为对象,研究了飞行高度、来流马赫数对边界层转捩位置等多个参数的影响.结果表明:随着飞行高度的增加,压缩面上边界层转捩位置延后,进气道总压恢复系数下降
Author:岳连捷
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