欢迎您!
东篱公司
退出
申报数据库
申报指南
立项数据库
成果数据库
期刊论文
会议论文
著 作
专 利
项目获奖数据库
位置:
成果数据库
>
会议
> 会议详情页
Experimental study of osculating inward turning cone waverider inlet forebody
所属机构名称:中国人民解放军国防科学技术大学
会议名称:2014 International hypersonic aircraft conference
时间:2014.6.15
成果类型:会议
相关项目:高超声速飞行器气动/推进/结构耦合问题研究
同会议论文项目
高超声速飞行器气动/推进/结构耦合问题研究
期刊论文 21
会议论文 14
同项目会议论文
Thermal-structural design of actively-cooled panels reinforced by light-weight truss cores
A theoretical and experimental study of the thermal buckling behaviour of the fully-clamped sandwich
Optimal design of actively-cooled panels strengthened with various cellular materials
基于3D-DIC的板壳结构热屈曲实验研究
Optimal design of actively-cooled panels strengthened with various cellular materials
主动冷却发动机壁板加强结构分析与设计
基于3D-DIC的板壳结构热屈曲实验研究
Osculating Inward turning Cone Waverider/Inlet (OICWI) Design and Experimental Study with Boundary L
Osculating inward turning cone waverider inlet design and experimental study with boundary layer cor
一种截面渐变三维内转式进气道的初步设计与评估
内外锥混压乘波前体进气道基准流场的设计与评估
Thermal-structural design of actively-cooled panels reinforced by light-weight truss cores
A theoretical and experimental study of the thermal buckling behaviour of the fully-clamped sandwich