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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：38/0  |  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：42/0  |  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：72/0  |  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：92/0  |  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：135/3  |  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：10/1  |  Submit date：2024/06/04
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./通讯作者：Wang, XY
Authors:  Wang XY(王小永);  Hong QZ(洪启臻);  Yang C(杨超);  Sun QH(孙泉华)
Adobe PDF(1380Kb)  |  Favorite  |  View/Download：108/15  |  Submit date：2023/06/15
Freestream Conditions  Reaction Rate Constant  Normal Shock Wave  Hypersonic Flows  
Learning Neural-Network-Based Turbulence Models for External Transonic Flows Using Ensemble Kalman Method 期刊论文
AIAA JOURNAL, 2023./通讯作者：Zhang, XL, He, GW
Authors:  Liu Y(刘毅);  Zhang XL(张鑫磊);  He GW(何国威)
Adobe PDF(8757Kb)  |  Favorite  |  View/Download：67/1  |  Submit date：2023/06/15
Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572./通讯作者：Yue, Lian-jie
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊);  Zhang QF(张启帆);  He CM(何成明)
Adobe PDF(6058Kb)  |  Favorite  |  View/Download：231/64  |  Submit date：2022/11/28
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946./通讯作者：Wang YP(汪运鹏)(1,2)
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：384/110  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering