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Robust Equivalent Source Method Based on Filtered Pressure for Aerodynamic Sound Prediction 期刊论文
AIAA JOURNAL, 2025, 卷号: 63, 期号: 3, 页码: 1203-1208./通讯作者：王士召
Authors:  Zhou ZT(周志腾);  Zang ZY(臧振宇);  Liu Y(刘毅);  Wang SZ(王士召)
Favorite  |  View/Download：2/0  |  Submit date：2025/03/21
Combustion Hysteresis Phenomenon in a Dual-Mode Scramjet 期刊论文
AIAA JOURNAL, 2024, 页码: 14./通讯作者：Yao, Wei
Authors:  Wang, Yu;  Yao W(姚卫);  Zhang, Zheng;  Liu, Jianwen
Favorite  |  View/Download：34/0  |  Submit date：2025/01/13
Combustion hysteresis  Dual-mode scramjet  Hydrogen fuels  IDDES  
An Explicit Algebraic Stress-Based Delayed Detached Eddy Simulation Model for Turbulent Flows 期刊论文
AIAA JOURNAL, 2024, 页码: 12./通讯作者：Yin, Zifei
Authors:  Liu HC(刘昊辰);  Zhang XL(张鑫磊);  Yin,Zifei;  He GW(何国威)
Favorite  |  View/Download：17/0  |  Submit date：2025/01/06
Computational Fluid Dynamics  Detached Eddy Simulation  Algebraic Reynolds Stress Model  Turbulence Models  Separated Flows  Turbulent Boundary Layer  
Reinforcement Learning for Submodel Assignment in Adaptive Modeling of Turbulent Flames 期刊论文
AIAA JOURNAL, 2024, 页码: 9./通讯作者：Ren, Zhuyin
Authors:  Yang TW(杨天威);  Yin,Yu;  Liu QL(刘起立);  Yu,Tao;  Wang,Yuwang;  Zhou,Hua;  Ren,Zhuyin
Favorite  |  View/Download：53/0  |  Submit date：2024/12/23
Reinforcement Learning  Thermoacoustic Combustion Instabilities  Computational Fluid Dynamics  Artificial Neural Network  Propulsion and Power  Turbulent Reacting Flow  High Performance Computing  Diffusion Flames  Numerical Combustion  
Kinetic Simulation of Nozzle Flow in a Micronewton-Class Cold Gas Thruster 期刊论文
AIAA JOURNAL, 2024, 页码: 10./通讯作者：Li, Yong, Hu, Yuan
Authors:  Sun WJ(孙文进);  Liu, Xuhui;  Long, Jun;  Wang, Xudong;  Sun QH(孙泉华);  Huang HJ(黄河激);  Li, Yong;  Hu Y(胡远)
Favorite  |  View/Download：84/0  |  Submit date：2024/10/08
Direct Simulation Monte Carlo  Micro Thruster  Variable Thrust  Multiscale Flow  Continuum Breakdown  
Experimental Study on Aerodynamic Heating of Hypersonic Boundary-Layer Blowing 期刊论文
AIAA JOURNAL, 2024, 页码: 6./通讯作者：Han, Guilai
Authors:  Li ZX(李宗贤);  Liu MK(刘美宽);  Han GL(韩桂来);  Wang DG(王大高);  Jiang ZL(姜宗林)
Favorite  |  View/Download：93/0  |  Submit date：2024/10/08
Heat Flux Distribution  Adverse Pressure Gradient  Aerodynamic Heating  Hypersonic Boundary Layer  Wind Tunnel Tests  Boundary Layer Control  
Representation of Thermomechanical Damage in Fiber-Reinforced Ceramic Composites at High Thermal Gradients 期刊论文
AIAA JOURNAL, 2024, 页码: 11./通讯作者：Yang, Zhengmao, Jiao, Jian
Authors:  Wang JT(王江涛);  Yang ZM(杨正茂);  Yue LJ(岳连捷);  Yang, Rui;  Jiao, Jian
Favorite  |  View/Download：95/0  |  Submit date：2024/06/11
Thermodynamic Properties  
Experimental Study on Supersonic Combustion Characteristics of Al/B-Kerosene Nanofuels 期刊论文
AIAA JOURNAL, 2024, 页码: 9./通讯作者：Zhong, Fengquan
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Gao ZB(高占彪)
Favorite  |  View/Download：110/0  |  Submit date：2024/05/21
Plasma Assisted Combustion  Petroleum  Nanomaterials  Supersonic Combustor  Flow Measurement  Optical Properties  Boundary Layers  Hydrocarbon Fuels  Band Pass Filter  Heat and Mass Transfer  
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8./通讯作者：Wang, Qiu
Authors:  Wang WT(王文韬);  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Gao, Liangjie;  Liu, Zhongchen;  Qian, Zhansen
Adobe PDF(2024Kb)  |  Favorite  |  View/Download：195/36  |  Submit date：2024/02/26
Finite Element Method  Hypersonic  Shock Tube/Tunnel  Diaphragm  Burst Pressure  
Similarity Analysis for Two-Dimensional Hypersonic Inlets Restart 期刊论文
AIAA Journal, 2023, 卷号: 61, 期号: 10, 页码: 4230-4246./通讯作者：岳连捷
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊)
Adobe PDF(1241Kb)  |  Favorite  |  View/Download：49/32  |  Submit date：2024/06/04
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