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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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State Key ... [4]
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朱兴坤 [4]
李新亮 [4]
唐志共 [3]
童福林 [3]
黄江涛 [2]
于长平 [1]
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2016 [3]
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中文 [4]
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航空学报 [3]
第八届全国高超声速科... [1]
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Creator:李新亮
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Language:中文
Author:李新亮
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转捩对压缩拐角激波/边界层干扰分离泡的影响
期刊论文
航空学报, 2016, 卷号: 37, 期号: 10, 页码: 2909-2921
Authors:
童福林
;
李新亮
;
唐志共
;
朱兴坤
;
黄江涛
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View/Download:432/89
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Submit date:2016/12/04
压缩拐角激波与旁路转捩边界层干扰数值研究
期刊论文
航空学报, 2016, 卷号: 37, 期号: 12, 页码: 3588-3604
Authors:
童福林
;
唐志共
;
李新亮
;
吴晓军
;
朱兴坤
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Adobe PDF(2221Kb)
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View/Download:270/70
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Submit date:2017/12/26
压缩拐角
激波/边界层干扰
旁路转捩
脉动压力
摩阻
直接数值模拟
转捩对压缩拐角激波/边界层干扰分离泡的影响
期刊论文
航空学报, 2016, 卷号: 37, 期号: 10, 页码: 2909-2921
Authors:
童福林
;
李新亮
;
唐志共
;
朱兴坤
;
黄江涛
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Adobe PDF(1595Kb)
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View/Download:463/84
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Submit date:2017/02/24
Transition
Compression Ramp
Shock Wave/boundary Layer Interaction
Separation Bubble
Direct Numerical Simulation
壁温对激波-湍流边界层干扰的影响规律研究
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
朱兴坤
;
于长平
;
李新亮
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Adobe PDF(631Kb)
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View/Download:351/133
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Submit date:2016/08/16
湍流边界层
壁温
恢复温度
绝热壁
压缩性效应
直接数值模拟
半经验公式
湍动能
过渡区
理论分析