超声速气流中凹腔对液体横向射流雾化特性影响的研究

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1、分类号V435学号14010068UDC000密级公开工学硕士学位论文超声速气流中凹腔对液体横向射流雾化特性影响的研究硕士生姓名李晨阳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李清廉教授二〇一六年十二月超声速气流中凹腔对液体横向射流雾化特性影响的研究国防科学技术大学研究生院StudyonSprayCharacteristicofLiquidJetWithaCavityinSupersonicCrossflowCandidate：LiChenyangAdvisor：Prof.LiQinglianAdisserta

2、tionSubmittedinpartialfulfillmentoftherequirementsforthedegreeofMasterofEngineeringinAeronauticalandAstronauticalScienceandTechnologyGraduateSchoolofNationalUniversityofDefenseTechnologyChangsha，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表目录........................................................................................................................III图目录................................

4、........................................................................................IV摘要...........................................................................................................................iABSTRACT..........................................

5、...........................................................................ii第一章绪论..................................................................................................................11.1研究背景与意义...........................................................

6、....................................11.2国内外研究进展...............................................................................................21.2.1射流空间分布研究进展........................................................................21.2.2射流雾化特性研究进展....................

7、....................................................41.2.3凹腔对射流影响研究进展....................................................................91.3本文研究的主要内容.....................................................................................12第二章试验与数值仿真研究方法...............

8、.............................................................132.1试验系统....................................................................