高超声速飞行器体襟翼气动热弹性耦合建模与分析.pdf

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1、分类号V215学号13019012ＵＤＣ密级公开工学博士学位论文高超声速飞行器体襟翼气动热弹性耦合建模与分析博士生姓名霍霖学科专业航空宇航科学与技术研究方向导弹总体设计与多场耦合仿真指导教师杨涛教授国防科学技术大学研究生院二〇一七年四月CoupledAerothermoelasticModelingandAnalysisofFlapforHypersonicVehiclesCandidate：HuoLinSupervisor：YangTaoAdissertationSubmittedinpartialfulfillment

2、oftherequirementsfortheprofessionaldegreeofDoctorofEngineeringinAeronauticalandAstronauticalScienceandTechnologyGraduateSchoolofNationalUniversityofDefenseTechnologyChangsha，Hunan，P.R.ChinaApril,2017国防科学技术大学研究生院博士学位论文国防科学技术大学研究生院博士学位论文目录摘要.........................

3、......................................................................................................iAbstract............................................................................................................................iii第一章绪论.....................

4、.............................................................................................11.1研究背景与意义.............................................................................................11.2关键技术及其相关研究进展...................................................

5、......................21.2.1动网格技术............................................................................................21.2.2数据接口技术........................................................................................71.2.3超声速非定常气动力工程算法-活塞理论...............

6、..........................101.2.4气动热弹性多场耦合..........................................................................111.3论文主要内容及其组织结构.......................................................................15第二章耦合边界数据接口技术研究...........................................

7、.............................172.1数据交互算法...............................................................................................172.1.1最近邻点插值法..................................................................................172.1.2径向基函数法....................

8、..................................................................172.1.3常体积转换法.........................................................................