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Display Method:
Studies on aerospike nozzle design and performance validation
WANG Chang-hui, LIU Yu, QIN Li-zi
2008, 26(2): 139-144.
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Design & dvelopment of a new captive trajectory simulation system in FL-24 wind tunnel
HUANG Xu-hui, LUO Xin-fu, YU Zhi-song
2008, 26(2): 145-149.
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An investigation of the airframe-inlet integration flow characteristics
YU Xin-hua, MA Jing-zhong, HU Zhu-gen, LI Xian-ping
2008, 26(2): 150-155,.
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Modeling and analytical investigation on rotor/wing aerodynamic interaction for tiltrotor aircraft
LI Chun-hua, XU Guo-hua
2008, 26(2): 156-162.
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Numerical analysis of thermal and chemical non-equilibrium testing flow-field around the reentry blunt body
DONG Wei-zhong, GAO Tie-suo, Zhang Zhi-cheng
2008, 26(2): 163-166.
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Large eddy simulation of 3-dimensional incompressible flow around a square cylinder
DENG Xiao-bing, ZHANG Han-xin, LI Qin
2008, 26(2): 167-172.
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Steady flow test and three-dimension numerical simulation of tumble flow in engine cylinder
Xu Yu-liang, Fu Guang-qi, Zu Bing-feng, Kang Xiu-ling, Liu Jie
2008, 26(2): 173-177,.
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The effect of relative thickness to the dynamic aerodynamic characteristics about pitching airfoils
Ran Jing-hong, Liu Zi-qiang, Bai Peng
2008, 26(2): 178-185.
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The numerical analysis of the effect of the pitching dynamic stability to the landing attitude for plane and blunt nose bomb
YUAN Xian-xu, YANG Ming-zhi, TANG Wei, CHEN Jian-qiang
2008, 26(2): 186-191.
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Flight dynamic mathematical model of tiltrotor aircraft
Song Yan-guo, Wang Huan-jin, Sha Hong-wei, Xu Min
2008, 26(2): 192-196.
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The image processing of phase change thermography
REN Xiao-Dong, HUANG Guo-Chuan, WANG Xiao-Nian, FENG Zu-Ren
2008, 26(2): 197-202.
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Investigation of internal compression flowfield for internal waverider-derived inlet
YOU Yan-cheng, LIANG De-wang
2008, 26(2): 203-207.
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Spinning effect on the flow of exhaust in combustion chamber of a solid rocket motor
Wang Ge, Chen Liang, Gao Ye, Gu Xuan
2008, 26(2): 208-211,.
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Numerical methods with modfied scheme for skew grids of low speed flow and its applications
LI Shu-min, ZHU Guo-lin, Wang Kai-chun
2008, 26(2): 212-216.
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Aerodynamic configuration conceptual design for a wing-body vehicle
TANG Wei, GUI Ye-wei, WANG An-ling, GAO Xiao-cheng
2008, 26(2): 217-220.
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Numerical research on separated flow around a WIG craft flying over wavy ground at high incidence angle
QU Qiu-lin, LIU Pei-qing, QIN Xu-guo
2008, 26(2): 221-226.
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An uncoupled method for numerical simulation of the nonequilibrium flow in COIL
Zhang Li, Ye Zheng-yin, Wang Gang
2008, 26(2): 227-230.
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An analysis of flow field characteristic for an advanced configuration aircraft during aerial refueling
L(U) Mei-qian, CHENG Cun-hu
2008, 26(2): 231-233.
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An investigation on controlling lateral characteristics for a flying wing configuration
Zhao Xia, Qin Yan-hua
2008, 26(2): 234-238.
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Numerical simulation on unsteady aerodynamics of rectangular flapping wing at low Reynolds number for micro air vehicle (MAVs)
SONG Shu-heng, ZHU Guo-lin, ZHANG Shu-hai
2008, 26(2): 239-245.
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A new idea of aerodynamic configuration for maneuvering warhead design
He Zheng-chun, He Kai-feng, Zhu Guo-lin
2008, 26(2): 246-248,.
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A new Jacobian matrix splitting method for idea MHD equations
Pan Yong, Wang Jiang-feng, Wu Yi-zhao
2008, 26(2): 249-256.
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Finite length microchannel flow in transitional regime (-Analytical prediction compared with experiment)
SHEN Ching, JIANG Jian-zheng
2008, 26(2): 257-262.
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Experimental studies on flight performances of spherical fragment
TAN Duo-wang, WEN Dian-ying, ZHANG Zhong-bin
2008, 26(2): 263-266.
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Statistical analysis of the articles published on ATCA Aerodynamica Sinica from 1997 to 2006
XU Yan, JIA Feng, LIU Lan-fang
2008, 26(2): 267-274.
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