Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 22 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
基于多层分块算法的激波干扰流场预测 期刊论文
力学学报, 2021, 卷号: 53, 期号: 12, 页码: 3284-3297
Authors:  李帅;  彭俊;  罗长童;  胡宗民
Adobe PDF(2372Kb)  |  Favorite  |  View/Download：222/68  |  Submit date：2022/03/16
激波干扰  高温气体效应  多层分块算法  高超声速流动  气动热  
Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  Favorite  |  View/Download：226/49  |  Submit date：2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
Adobe PDF(4178Kb)  |  Favorite  |  View/Download：310/75  |  Submit date：2021/11/15
Strain  Balance  Milli-newton  Design  Calibration  
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  Favorite  |  View/Download：314/59  |  Submit date：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
Authors:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
Adobe PDF(8485Kb)  |  Favorite  |  View/Download：132/68  |  Submit date：2022/10/25
SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  Favorite  |  View/Download：327/61  |  Submit date：2022/01/12
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  Favorite  |  View/Download：283/109  |  Submit date：2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15
Authors:  Zhao, Cheng;  Yang Y(杨焱);  Zhang, Tao;  Dong, Haibo;  Hou, Guoxiang
Adobe PDF(3919Kb)  |  Favorite  |  View/Download：325/79  |  Submit date：2021/08/30
Acoustic perturbation equations  Immersed boundary method  Flow-induced noise  Four-cylinder array  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  Favorite  |  View/Download：342/52  |  Submit date：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
高超声速MHD球头激波脱体距离理论求解 期刊论文
力学学报, 2021, 卷号: 53, 期号: 09, 页码: 2493-2500
Authors:  李逸翔;  汪球;  罗凯;  李进平;  赵伟
Adobe PDF(1290Kb)  |  Favorite  |  View/Download：240/53  |  Submit date：2021/11/12
高超声速  磁流体动力学  激波脱体距离  流动控制