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| Analysis of the test condition of a shock-expansion tube: JF-16 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012-10
作者: Hu ZM(胡宗民) ; Wu B(吴波); Jiang ZL(姜宗林)
 Adobe PDF(264Kb) |  收藏 | 浏览/下载：835/247 | 提交时间：2013/03/16
Shock-expansion Tube Computation Spurious Oscillation Flus Splliting |
| The applicability of Mach number independence principle in case of hypersonic thermo-chemical nonequilibrium flow 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012
作者: Li K(李康); Li JP(李进平); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(1755Kb) | 收藏 | 浏览/下载：622/140 | 提交时间：2015/03/02
Keywords: Mach Number Independence Oswatitsch Nonequilibrium Flow Real-gas Effect Expansion Effect |
| Vortex generation arising from the interaction of shock wave and fuel bubble 会议论文
The Sixth Across-strait Workshop on Shock/Vortex Interaction, Guiyang, 2012-07
作者: Hu ZM(胡宗民); Jiang ZL(姜宗林); Dou HS
Adobe PDF(309Kb) | 收藏 | 浏览/下载：703/125 | 提交时间：2013/03/16 |
| CFD for chemically reacting flow and its applications 会议论文
International Conference on Advanced Aircraft Technologies 2012, South Korea, 2012-5
作者: Hu ZM(胡宗民); Sun XF; Jiang ZL(姜宗林)
Adobe PDF(1482Kb) | 收藏 | 浏览/下载：603/144 | 提交时间：2013/03/16 |
| A New Non-ablative TPS for Hypersonic Vehicles 会议论文
第十五届全国激波与激波管学术会议（上册）, 中国浙江杭州, 2012-07-13
作者: Liu YF(刘云峰); Jiang ZL(姜宗林)
浏览 | Adobe PDF(985Kb) | 收藏 | 浏览/下载：183/61 | 提交时间：2015/09/10
Hypersonic Flow Tps Shock Wave Drag Reduction |
