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| Recent Progress of Microgravity Science Research in China 期刊论文 空间科学学报, 2022, 卷号: 42, 期号: 4, 页码: 772-785 作者: Zhao JF(赵建福); Du WF(杜王芳); Kang Q(康琦); Lan D(蓝鼎); Li K(李凯); Li WB(李伟斌); Liu YC; Luo XH; Miao JY; Wang QG; Wang SF(王双峰); Zhang T; Zhang XW; Zhang YH; Zheng HQ Adobe PDF(2911Kb)  |  收藏  |  浏览/下载:162/63  |  提交时间:2023/03/16 |
| Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 14 作者: Zhou, Lin; Teng, Honghui; Ng, Hoi Dick; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(6382Kb)  |  收藏  |  浏览/下载:219/32  |  提交时间:2021/11/01 Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文 JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12 作者: Shi Weixiu; Pan LS(潘利生); Jin Suyi; Dong YH(董跃华); Li T(李腾); Zhao J(赵京); Wei XL(魏小林) Adobe PDF(2198Kb)  |  收藏  |  浏览/下载:237/51  |  提交时间:2021/11/01 CO2-based mixture flammability laminar flame speed flammable critical mixing ratio transcritical power cycle |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 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) Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:280/55  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:383/57  |  提交时间:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:322/169  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 作者: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:252/101  |  提交时间:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475 作者: Wang Q(汪球); Luo K(罗凯); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2057Kb)  |  收藏  |  浏览/下载:253/79  |  提交时间:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177 作者: Yao W(姚卫) Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:645/293  |  提交时间:2019/12/17 Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| Non-premixed turbulent combustion modeling based on the filtered turbulent flamelet equation 期刊论文 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 63, 期号: 4, 页码: 6 作者: Zhang J(张健); Wang LP; Guo YQ Adobe PDF(1505Kb)  |  收藏  |  浏览/下载:170/52  |  提交时间:2020/05/18 turbulent combustion modeling turbulent flamelet equation large eddy simulation non-premixed flame |