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An analytical model for maximum temperature and temperature distribution of plate structure with active cooling 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 5, 页码: 322290
作者:  Hu GH(胡国豪);  Zhong FQ(仲峰泉);  Chen KT(陈科挺)
Adobe PDF(2013Kb)  |  收藏  |  浏览/下载：49/0  |  提交时间：2023/04/20
Plate structure  Active cooling  Thermal protection  Convective heat transfer  Analytical model  
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  
A new dynamic subgrid-scale model using artificial neural network for compressible flow 期刊论文
THEORETICAL AND APPLIED MECHANICS LETTERS, 2022, 卷号: 12, 期号: 4
作者:  Qi H(齐涵);  Li XL(李新亮);  Luo, Ning;  Yu ZP(于长平)
Adobe PDF(2851Kb)  |  收藏  |  浏览/下载：39/10  |  提交时间：2024/01/15
Subgrid-scale kinetic energy  Eddy-viscosity model  Compressible flow  
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
作者:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(2084Kb)  |  收藏  |  浏览/下载：342/77  |  提交时间：2020/07/06
Large-eddy simulation  Subgrid-scale model  Rotating turbulent channel flow  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1080Kb)  |  收藏  |  浏览/下载：512/126  |  提交时间：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
高压捕获翼位置设计方法研究 期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 576-584
作者:  李广利;  崔凯;  肖尧;  徐应洲
浏览  |  Adobe PDF(992Kb)  |  收藏  |  浏览/下载：408/63  |  提交时间：2016/12/16
High-speed Vehicles  High Pressure Capturing Wing  Uniform Experimental Design  Polynomial Surrogate Model  
高压捕获翼前缘型线优化和分析 期刊论文
力学学报, 2016, 卷号: 48, 期号: 4, 页码: 877-885
作者:  李广利;  崔凯;  肖尧;  徐应洲
浏览  |  Adobe PDF(944Kb)  |  收藏  |  浏览/下载：322/60  |  提交时间：2016/12/16
High Pressure Capturing Wing  Computational Fluid Dynamic  Surrogate Model  Shape Optimization  
On the validity of the Boltzmann-BGK model through relaxation evaluation 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 2, 页码: 133-143
作者:  Sun QH(孙泉华);  Cai CP;  Gao W(高巍);  Sun, QH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载：853/233  |  提交时间：2014/06/05
Bgk Model  Boltzmann Equation  Validity Evaluation  Dsmc Method  Time Relaxation  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
作者:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  收藏  |  浏览/下载：869/282  |  提交时间：2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models  
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
作者:  Lin X;  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(828Kb)  |  收藏  |  浏览/下载：799/241  |  提交时间：2013/01/18
Radiation Measurements  Shock Wave  Mars Re-entry  Rotational Temperature  Vibrational Temperature  Radiation Measurements  Cn  Entry  Tube  Mixtures  Model