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DeepStSNet: Reconstructing the quantum state-resolved thermochemical nonequilibrium flowfield using deep neural operator learning with scarce data 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2023, 卷号: 491, 页码: 112344
作者:  Lv JQ(吕家琦);  Hong QZ(洪启臻);  Wang XY(王小永);  Mao, Zhiping;  Sun QH(孙泉华)
Adobe PDF(5558Kb)  |  收藏  |  浏览/下载:64/0  |  提交时间:2023/09/26
Hypersonic  Thermochemical nonequilibrium  State-to-state approach  Deep learning  Multiphysics  Data assimilation  
Stochastic simulation of hydrogen-oxygen auto-ignition at the microscale 期刊论文
JOURNAL OF CHEMICAL PHYSICS, 2023, 卷号: 159, 期号: 8, 页码: 84105
作者:  Yang C(杨超);  Hu Y(胡远);  Wang XY(王小永);  Hong QZ(洪启臻);  Sun QH(孙泉华)
Adobe PDF(8545Kb)  |  收藏  |  浏览/下载:41/0  |  提交时间:2023/09/26
Uncertainty Quantification in State-Specific Modeling of Thermal Relaxation and Dissociation of Oxygen 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 6, 页码: 2734-2738
作者:  Wang XY(王小永);  Hong QZ(洪启臻);  Yang C(杨超);  Sun QH(孙泉华)
Adobe PDF(1380Kb)  |  收藏  |  浏览/下载:62/0  |  提交时间:2023/06/15
Freestream Conditions  Reaction Rate Constant  Normal Shock Wave  Hypersonic Flows  
On the accuracy of two temperature models for hypersonic nonequilibrium flow 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 2, 页码: 122193
作者:  Wang XY(王小永);  Hong QZ(洪启臻);  Hu Y(胡远);  Sun QH(孙泉华)
Adobe PDF(2067Kb)  |  收藏  |  浏览/下载:51/0  |  提交时间:2023/04/20
Nonequilibrium flow  Two temperature model  Quasi classical trajectory  Non Boltzmann effect  Vibration dissociation coupling effect  
On the Reynolds-Number Sensitivity of Inlet Flow at Mach Numbers Beyond 7 期刊论文
AIAA JOURNAL, 2022, 卷号: 60, 期号: 3, 页码: 1978-1982
作者:  Chen H(陈昊);  Wang ZR;  Zhang QF(张启帆);  Zhang XY(张晓源);  Yue LJ(岳连捷)
Adobe PDF(625Kb)  |  收藏  |  浏览/下载:111/27  |  提交时间:2022/10/25
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  收藏  |  浏览/下载:376/61  |  提交时间:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
作者:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:236/34  |  提交时间:2021/11/12
高速进气道  低马赫数不起动  非定常  气动力  自起动  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  收藏  |  浏览/下载:186/44  |  提交时间:2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  收藏  |  浏览/下载:253/103  |  提交时间:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
作者:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:200/48  |  提交时间:2021/01/12