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| 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
Authors: Jiang ZL(姜宗林) ; Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
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High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Specific signal imaging velocimetry for rarefied plasma flows 期刊论文
EXPERIMENTS IN FLUIDS, 2020, 卷号: 61, 期号: 12, 页码: 247
Authors: Cao JW(曹进文); Huang HJ(黄河激); Pan WX(潘文霞); Meng X(孟显); Wu CK(吴承康)
Adobe PDF(4736Kb) | Favorite | View/Download：296/89 | Submit date：2020/12/28
MOLECULAR TAGGING VELOCIMETRY MACH PROBE VELOCITY TURBULENT JETS |
| 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
Authors: 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)
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hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| 微波对超声速燃烧影响实验研究 学位论文
硕士论文，北京: 中国科学院大学, 2020
Authors: 孙文明
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微波 超声速燃烧 火焰速度 火焰位置 火焰稳定性 |
| An improved weighted essentially non-oscillatory scheme with modified smoothness indicator tau and adaptive index p 期刊论文
INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 2020, 页码: 15
Authors: Li X(李欣); Yu ZP(于长平); Li L; Li XL(李新亮)
Adobe PDF(3965Kb) | Favorite | View/Download：301/104 | Submit date：2020/06/15
WENO scheme high resolution shock-capturing smoothness indicator adaptive optimisation |
