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The effects of physicochemical models on distribution of plasma in high temperature flowfield
GAO Tie-suo, DONG Wei-zhong, DING Ming-song, JIANG Tao
2013, 31(5): 541-545. DOI: 10.7638/kqdlxxb-2011.0190
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Application of harmonic balance method in forward flight simulation for helicopter rotors
XU Jian-hua, SONG Wen-ping, WANG Long
2013, 31(5): 546-553. DOI: 10.7638/kqdlxxb-2011.0121
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Numerical study on flow structure over a delta wing
ANG Yun-tao, ZHANG Yu-lun, WANG Guang-xue, DENG Xiao-gang
2013, 31(5): 554-558. DOI: 10.7638/kqdlxxb-2012.0001
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Study on static aerothermoelasticity for hypersonic vehicle
LIU Lei, GUI Ye-wei, GENG Xiang-ren, TANG Wei, WANG An-ling
2013, 31(5): 559-563. DOI: 10.7638/kqdlxxb-2012.0006
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Analysis of rotor wake stability in hovering state by Fourier method
Lü Wei-liang, ZHAO Qi-jun, XU Guo-hua
2013, 31(5): 564-571. DOI: 10.7638/kqdlxxb-2012.0008
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The experimental study of aerodynamics and flow structures of a wing with Gurney flaps in ground effect
XIAO Tao, Daichin
2013, 31(5): 572-578. DOI: 10.7638/kqdlxxb-2012.0053
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Aerodynamic characteristics of CRH2 train in combination of vehicle-bridge with cross wind action
LI Yong-le, XIANG Huo-yue, HOU Guang-yang, CHEN Ke-jian
2013, 31(5): 579-582. DOI: 10.7638/kqdlxxb-2011.0127
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The aerodynamic design of seamlessly camber-variable airfoil based on circulation control
KONG Bo, WANG Fu-xin, ZHOU Tao
2013, 31(5): 583-586. DOI: 10.7638/kqdlxxb-2011.0187
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Drag reduction investigation on high wing aircraft landing gear fairing
ZHANG Xiao-min, WANG Fu-xin, SUN Wei-ping, QI yang
2013, 31(5): 587-591. DOI: 10.7638/kqdlxxb-2011.0199
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Numerical prediction of the effects of condensation of moist air on the aerodynamic characteristics of the RAE 2822 airfoil
SUN Xiu-ling, MA Xiao-yong, LI Liang, LI Guo-jun
2013, 31(5): 592-597. DOI: 10.7638/kqdlxxb-2011.0202
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Jet flow involved numerical simulation of missile launching from the R/S UAV
ZHU Bing, ZHU Xiao-ping, XU Xiao-ping, XIONG Lei
2013, 31(5): 598-603. DOI: 10.7638/kqdlxxb-2011.0205
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Application of γ-Reθt-SA transition model in numertical simulation of flows around airfoils
ZHU Jun, GAO Zheng-hong, BAI Jun-qiang, ZHAN Hao
2013, 31(5): 604-610. DOI: 10.7638/kqdlxxb-2011.0211
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A contrastive study of different time interval moving average statistical characteristics of strong wind near ground
SHI Wen-hai, LI Zheng-nong, WU jian-jia
2013, 31(5): 611-615. DOI: 10.7638/kqdlxxb-2011.0309
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The impact of ice thickness on the aerodynamic characteristics of crescent shape iced conductors
LOU Wen-juan, LIN Wei, HUANG Ming-feng, SHEN Guo-hui, CHEN Yong, YAN Dong
2013, 31(5): 616-622. DOI: 10.7638/kqdlxxb-2011.0315
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Effects of continuum breakdown on aerodynamics of near space vehicle
HUANG Fei, ZHANG Liang, CHENG Xiao-li, SHEN Qing
2013, 31(5): 623-628. DOI: 10.7638/kqdlxxb-2012.0002
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Design and aerodynamic performance of a M shaped inlet on flying wing UAV
YU Xin-hua
2013, 31(5): 629-634. DOI: 10.7638/kqdlxxb-2012.0009
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High skewness tetrahedron meshes and its application on high lift configuration
XIAO Zhong-yun, LIU Gang, ZHOU Zhu, JIANG Xiong
2013, 31(5): 635-640. DOI: 10.7638/kqdlxxb-2012.0010
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Surrogatebased optimization of 3D afterbody nozzle
MIAO Meng, , ZENG Peng
2013, 31(5): 641-646. DOI: 10.7638/kqdlxxb-2012.0011
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Flow control of different plasma actuations over a slender conical forebody
MENG Xuan-shi, WANG Jian-lei, CAI Jin-sheng, LUO Shi-jun, LIU Feng
2013, 31(5): 647-651.
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Numerical simulation about grid fin’s dynamic characteristic by patched mesh
CHEN Jian-zhong, ZHANG Zhao, HUANG Guo-chuan
2013, 31(5): 652-656. DOI: 10.7638/kqdlxxb-2012.0038
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Numerical research on interior ballistics of the launch process of two-stage light gas gun
HUANG Jie, LIANG Shi-chang, LI Hai-yan, LIU Sen
2013, 31(5): 657-661. DOI: 10.7638/kqdlxxb-2012.0055
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pplication of CE/SE method using triangular meshes on calculation two-phase pulse detonation engine with nozzle
WANG Yan-yan, WENG Chun-sheng
2013, 31(5): 662-669. DOI: 10.7638/kqdlxxb-2012.0077
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Time spectral method for unsteady viscous flow around an oscillating airfoil
CHENG Su-kun, YANG Xiao-quan, YANG Ai-ming
2013, 31(5): 670-675. DOI: 10.7638/kqdlxxb-2012.0035
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Advances in the aerodynamics research of cylcoidal propeller
TANG Ji-wei, HU Yu, SONG Bi-feng
2013, 31(5): 676-684. DOI: 10.7638/kqdlxxb-2013.0054
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