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Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
作者:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  收藏  |  浏览/下载：194/44  |  提交时间：2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
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：187/44  |  提交时间：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
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  
An Elasto-Plastic Damage Constitutive Theory Based on Pair Functional Potentials and Slip Mechanism 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2010, 卷号: 23, 期号: 6, 页码: 686-697
作者:  Liu F(刘芳);  Fu Q(付强);  Chen C(陈岑);  Liang NG(梁乃刚);  Liang, NG (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2771Kb)  |  收藏  |  浏览/下载：203/58  |  提交时间：2016/02/01
Elasto-plastic Damage Constitutive Relation  Finite Deformation  Pair Functional Potentials  Cauchy-born Rule  Slip Mechanism  Component Assembling Model