机构

• 力学研究所 [6]

采集方式

• OAI收割 [6]

内容类型

• 会议论文 [3]
• 期刊论文 [3]

发表日期

• 2022 [1]
• 2021 [1]
• 2015 [1]
• 2009 [1]
• 2003 [1]
• 2001 [1]
• 更多

学科主题

• Engineerin... [1]

筛选

浏览/检索结果: 共6条，第1-6条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor 期刊论文  OAI收割 ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16 作者:  Li, Zhen;  Gu, Hongbin;  Gu HB(顾洪斌);  Li Z(李桢)   |  收藏  |  浏览/下载：33/0  |  提交时间：2022/07/18 scramjet combustor  direct-connect test  jet scale  flame stabilization   Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文  OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)   |  收藏  |  浏览/下载：25/0  |  提交时间：2021/05/17 Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test   Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文  OAI收割 Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475 作者:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇) 收藏  |  浏览/下载：41/0  |  提交时间：2015/04/28 hypersonic scramjet test tunnel  nozzle  aerodynamic heating  convective heat transfer   Performance of the fuel injector in supersonic combustor 会议论文  OAI收割 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009 作者:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙) 收藏  |  浏览/下载：22/0  |  提交时间：2017/07/14 Concentration profiles  Engine design  Fuel injectors  Fuel-air mixing  Gas sampling  Ramp injector  Scramjet combustors  Scramjet test  Supersonic combustors   Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文  OAI收割 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003 作者:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇) 收藏  |  浏览/下载：23/0  |  提交时间：2017/06/01 Compressible Navier-Stokes  Computational studies  Experimental comparison  Experimental investigations  Flow charac-teristics  Hypersonic propulsion test facility  Performance parameters  Scramjet inlets   Development of the facility for model scramjet testing 会议论文  OAI收割 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001 作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴) 收藏  |  浏览/下载：27/0  |  提交时间：2017/06/01 Chinese Academy of Sciences  Enthalpy flow  Hypersonic propulsion test facility  Performance tests  Scramjet testing  Supersonic combustion  Total pressure  Total temperatures