激波-湍流边界层干扰流场壁温效应的直接数值模拟

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1、.分类号V411学号14010112UDC密级公开工学硕士学位论文激波/湍流边界层干扰流场壁温效应的直接数值模拟硕士生姓名朱轲学科专业航空宇航科学与技术研究方向高超声速推进技术指导教师刘卫东教授二〇一六年十一月Directnumericalsimulationonwall-temperatureeffectofshockwave/turbulentboundarylayerinteractionCandidate：ZhuKeAdvisor：Prof.LiuWeidongAdissertationSu

2、bmittedinpartialfulfillmentoftherequirementsforthedegreeofMasterofEngineeringinAeronauticalandAstronauticalScienceandTechnologyGraduateSchoolofNationalUniversityofDefenseTechnologyChangsha，Hunan，P.R.China（November，2016）国防科学技术大学研究生院硕士学位论文目录目录...........

3、....................................................................................................................I摘要.................................................................................................................................iABS

4、TRACT.....................................................................................................................ii第一章绪论....................................................................................................................11.1激波/

5、边界层干扰研究背景.................................................................11.1.1应用背景.......................................................................................11.1.2SWBLI概述....................................................................

6、...............21.2激波/边界层干扰国内外研究进展.....................................................41.2.1SWBLI实验研究进展...................................................................41.2.2SWBLI数值计算研究进展...........................................................61.

7、2.3SWBLI的壁温效应研究...............................................................91.2.4研究发展趋势..............................................................................101.3本文的主要研究内容......................................................................

8、..11第二章数值模拟方法介绍..........................................................................................132.1可压缩湍流直接数值模拟方法........................................................132.1.1可压缩N-S方程..........................................