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Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 3, 页码: 362-368
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Yang Y;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuan Xi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1122Kb)  |  Favorite  |  View/Download：382/103  |  Submit date：2016/09/14
3d Shock/shock Interaction  Mach Interaction  Spatial Dimension Reduction  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download：360/93  |  Submit date：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 4, 页码: 500-511
Authors:  Wu CK(吴承康);  Pan WX(潘文霞);  Meng X(孟显);  Wang, Hai-Xing;  Wu, CK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(878Kb)  |  Favorite  |  View/Download：471/130  |  Submit date：2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number  
Direct Numerical Simulation of Compressible Turbulent Flows 期刊论文
ACTA MECHANICA SINICA, 2010, 卷号: 26, 期号: 6, 页码: 795-806
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(2048Kb)  |  Favorite  |  View/Download：401/237  |  Submit date：2016/02/01
Direct Numerical Simulation  Compressible Turbulence  Coherent Structures  Turbulent Boundary-layer Flow