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Display Method:
The effects of Reynolds number on airplane aerodynamic characteristics
ZHANG Pei-hong, ZHOU Nai-chun, DENG You-qi, MA Ming-sheng
2012, 30(6): 693-698.
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平面定常跨声速等熵流动的分析
吴寿荣
2012, 30(6): 699-703.
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Experimental research on characteristic of turbulent kinetic energy at the interface between compressible mixing layer and free stream
GAN Cai-jun, WEI Lian-feng, LI Lang, MA Han-dong, XIONG Hong-liang
2012, 30(6): 704-708.
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Spectral property comparison of fifthorder nonlinear WCNS and WENO difference schemes
TU Guo-hua, , DENG Xiao-gang
2012, 30(6): 709-712.
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The investigation on the supersonic flow over three dimensional intersecting wedges
YANG Yang, TENG Hong-hui, JIANG Zong-lin
2012, 30(6): 713-718.
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Adjoint based on high precise aerodynamic shape optimization for transonic civil aircraft
WU Wen-hua, FAN Zhao-lin, CHEN De-hua, QIN Ning, MENG De-hong
2012, 30(6): 719-724.
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Numerical investigation of the powered effects on civil aircraft
JIA Hong-yin, DENG You-qi, MA Ming-sheng, ZHANG Yao-bing
2012, 30(6): 725-730.
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Energy release law of one-dimension pulse detonation wave
TENG Hong-hui, LIU Yun-feng, JIANG Zong-lin
2012, 30(6): 731-736.
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Simulation of equilibrium atmosphere boundary layer with SST k-ω turbulence model
HU Peng, LI Yong-le, LIAO Hai-li
2012, 30(6): 737-743.
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Investigation on aerodynamic characteristics of internal bay's door
WU Ji-fei, , XU Lai-wu, FAN Zhao-lin
2012, 30(6): 744-748.
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Application of inflow boundary conditions for DNS on bypass transition
LU Xue-zhi, HUANG Zhang-feng,
2012, 30(6): 749-753.
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The influences of Mach number on the supersonic flow past a 3D-rectangular cylinder mounted on a plane
XUE Da-wen, CHEN Zhi-hua, SUN Xiao-hui, HAN Jun-li
2012, 30(6): 754-760.
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Experimental and numerical study on hypersonic jaws inlet
WANG Cheng-peng, DONG Hao, CHENG Ke-ming
2012, 30(6): 761-766.
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Numerical investigations of formation mechanism about a dual leading edge vortex structure of a delta wing with medium leading edge sweep angle
LIU Jie, , LIU Pei-qing
2012, 30(6): 767-771.
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Effect of treatment for pressure derivate terms on the temporal accuracy of the projection method for unsteady flow
WU Shao-hua, ZHANG-Jian
2012, 30(6): 772-776.
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Experiment on aerodynamic characteristics of a novel micro tilt ducted fan aircraft with wings
CAI Hong-ming, ANG Hai-song, ZHANG Hua-liang, DUAN Wen-bo
2012, 30(6): 777-781.
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Numerical study of unsteady features of airflow around the Ahmed body
ZHU Hui,
2012, 30(6): 782-785.
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Numerical investigation on the mechanism of micro tab to the airfoil
WU Ya-dong, OUYANG Hua, XU Kun, TENG Jin-fang, DU Zhao-hui
2012, 30(6): 786-791.
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Relaxation based PTV with Delaunay triangulation
JIA Pan, WANG-Yuan, ZHANG-Yang
2012, 30(6): 792-797.
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Study on influence of brackets on the aerodynamic performance of high lift system
BAI Jun-qiang, QIU Ya-song, CHEN Ying-chun, LI Ya-lin, ZHOU Tao
2012, 30(6): 798-804.
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