Numerical Study on Drag Reduction by Micro-Blowing/Suction Compounding Flow Control on Supercritical Airfoil
Cai Junxuan , Gao Zhen Xun
Procedia Engineering 99 613 -617
18
2015
An Iterative Technique for Coupled Conduction–Radiation Heat Transfer in Semitransparent Media
Jing Ying Wang , Zhen Xun Gao , Chun Hian Lee
Numerical Heat Transfer Part A-applications 67 ( 11) 1208 -1231
3
2015
A new wall function boundary condition including heat release effect for supersonic combustion flows
Zhen-Xun Gao , Chong-Wen Jiang , Chun-Hian Lee
Applied Thermal Engineering 92 62 -70
10
2016
A hybrid numerical scheme for aeroheating computation of hypersonic reentry vehicles
Zhen-Xun Gao , Hai-Chao Xue , Zhi-Chao Zhang , Hong-Peng Liu
International Journal of Heat and Mass Transfer 116 432 -444
7
2018
Influence of inter-car wind-shield schemes on aerodynamic performance of high-speed trains
Jia-Shou Yang , Chong-Wen Jiang , Zhen-Xun Gao , Yu-Chao Lu
Journal of the China Railway Society 34 ( 11) 29 -35
16
2012
Numerical simulation of sand load applied on high-speed train in sand environment
Tian-tian Wang , Chong-wen Jiang , Zhen-xun Gao , Chun-hian LEE
Journal of Central South University 24 ( 2) 442 -447
5
2017
Unsteady characteristics of supersonic base flow influenced by the exhaust jet
Yu-yan Tian , Li-hui Shen , Zhen-xun Gao , Chong-wen Jiang
Physics of Fluids 36 ( 9)
2024
Numerical investigation of compressibility effects in turbulent channel flows using large eddy simulation
SuoZhu Wang , ZhenXun Gao , ChunHian Lee
Science China Physics, Mechanics and Astronomy 55 ( 2) 305 -315
7
2012
A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine
ZhenXun Gao , ChunHian Lee
Science China-technological Sciences 53 ( 8) 2111 -2121
52
2010
A flamelet model for turbulent diffusion combustion in supersonic flow
ZhenXun Gao , ChunHian Lee
Science China Technological Sciences 53 ( 12) 3379 -3388
14
2010
Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet
ZhenXun Gao , ChunHian Lee
Science China Technological Sciences 54 ( 4) 883 -893
39
2011
Improvement and application of wall function boundary condition for high-speed compressible flows
ZhenXun Gao , ChongWen Jiang , ChunHian Lee
Science China Technological Sciences 56 ( 10) 2501 -2515
42
2013
A decoupled procedure for convection-radiation simulation in scramjets
JingYing Wang , ZhenXun Gao , ChunHian Lee , HuiQiang Zhang
Science China Technological Sciences 57 ( 12) 2551 -2566
5
2014
Review of researches on compressible turbulent boundary layer combustion for skin friction reduction
LIU Hongpeng , GAO Zhenxun , JIANG Chongwen , LEE Chunhian
空气动力学学报 38 ( 3) 593 -602
3
2020
The progress of the overlapping grid techniques
LI Peng , GAO Zhenxun , JIANG Chongwen
Mechanics in Engineering 36 ( 5) 551 -565
14
2014
Investigation of pressure wave behaviors in the rotational speed effects on a pressure-exchange wave rotor
CHAN Shining , LIU Huoxing , SONG Hang , LI Fengchao
Chinese Journal of Aeronautics 35 ( 5) 247 -259
8
2022
Review of numerical simulation methods for hypersonic and high-enthalpy non-equilibrium flow
GAO Zhenxun , JIANG Chongwen , LI Chun-Xuan
力学进展 53 ( 3) 561 -591
1
2023
Direct design method for generating osculating curved wave-rider based on complex leading-edge profile
Chongwen Jiang , Zhihao Li , HU Shuyao , Chenhao Xu
2024
Oblong-shaped rotor engine having high sealing performance
Chongwen Jiang , PI Siyuan , Chenhao Xu , Zhihao Li
2023
Progress of the studies on the extension of flamelet models to supersonic combustion flows
GAO Zhenxun , JIANG Chongwen , LEE Chunhian
ACTA AERODYNAMICA SINICA 38 ( 4) 651 -659
2020