2005 No. 2

Display Method:
Investigation of flow field characteristics on a slender body at high angle of attack
GU Yun-song, MING Xiao
2005, 19(2): 1-6. doi: 10.3969/j.issn.1672-9897.2005.02.001
Abstract(121) PDF(4)
Abstract:
Experimental study of different leading-edge profiles of a 40 degree-sweep delta wing
BAI Tao, WANG Jin-jun
2005, 19(2): 7-10,19. doi: 10.3969/j.issn.1672-9897.2005.02.002
Abstract(127) PDF(3)
Abstract:
Investigation of kerosene jet spray in supersonic combustion
WANG Dong, YU Gong
2005, 19(2): 11-13. doi: 10.3969/j.issn.1672-9897.2005.02.003
Abstract(160) PDF(5)
Abstract:
Investigation of flow field of methane-air the secondary explosion
JIANG Xiao-hai, FAN Bao-chun, YE Jing-fang
2005, 19(2): 14-19. doi: 10.3969/j.issn.1672-9897.2005.02.004
Abstract(92) PDF(4)
Abstract:
A mathematical method for calculating the three stresses on turbine blade from axiom of sine function at every angle
YANG Jian-xin, YANG Gui-wen
2005, 19(2): 20-27,39. doi: 10.3969/j.issn.1672-9897.2005.02.005
Abstract(86) PDF(2)
Abstract:
Computations of airfoil dynamic responses based on unsteady aerodynamic model
SONG Chen-yao, XU Guo-hua
2005, 19(2): 28-34. doi: 10.3969/j.issn.1672-9897.2005.02.006
Abstract(101) PDF(3)
Abstract:
Laser shadowgraph for the visualization of hypervelocity impact debris cloud
Liu Sen, XIE Ai-min, HUANG Jie, LI Yi, LUO Jin-yang, SHI An-hua
2005, 19(2): 35-39. doi: 10.3969/j.issn.1672-9897.2005.02.007
Abstract(85) PDF(7)
Abstract:
Experimental technique on direct measuring of aerodynamic forces of airfoil
JIAO Yu-qin, ZHANG Bin-qian, JIN Cheng-xin, DUAN Zhuo-yi, YU Xin
2005, 19(2): 40-44. doi: 10.3969/j.issn.1672-9897.2005.02.008
Abstract(83) PDF(5)
Abstract:
Arc plasma supersonic nozzle flow device with high stability
Yue Bin, LE Jia-ling, BAO Wei-yi
2005, 19(2): 45-48. doi: 10.3969/j.issn.1672-9897.2005.02.009
Abstract(102) PDF(5)
Abstract:
Application of improved neural networks to cascade aerodynamic experiment
YANG Bo, HAN Hai-quan, GU Chuan-Gang
2005, 19(2): 49-54,59. doi: 10.3969/j.issn.1672-9897.2005.02.010
Abstract(113) PDF(2)
Abstract:
Investigation of aerodynamic characteristics of tunnel portals in high-speed railway
ZHAO Wen-cheng, GAO Bo, ZHENG Chang-qing, ZHANG Zhao-jie
2005, 19(2): 55-59. doi: 10.3969/j.issn.1672-9897.2005.02.011
Abstract(100) PDF(2)
Abstract:
Experiments on the drag-reduction of non-wetting materials
YU Yong-sheng, WEI Qing-ding
2005, 19(2): 60-66. doi: 10.3969/j.issn.1672-9897.2005.02.012
Abstract(123) PDF(6)
Abstract:
"The single circuit" method and its application in measure of scoop's power consumption in high-speed gas centrifuge
WEN Bao-lian, TU Guang-bei, ZHANG Wei, SONG Ding
2005, 19(2): 67-70. doi: 10.3969/j.issn.1672-9897.2005.02.013
Abstract(94) PDF(2)
Abstract:
Application of scan pitot-pressure rake in hypersonic propulsion wind tunnel flow field measurement
CHANG Yuan, GU Hong-bin, CHEN Li-hong, ZHANG Xin-yu
2005, 19(2): 71-73,83. doi: 10.3969/j.issn.1672-9897.2005.02.014
Abstract(117) PDF(8)
Abstract:
Measurements of cylinder's wake by PIV
ZHANG Xiao-di, JIANG Jia-li, JIA Yuan-sheng, MA Hong-zhi, XIAO Ya-ke
2005, 19(2): 74-78. doi: 10.3969/j.issn.1672-9897.2005.02.015
Abstract(93) PDF(7)
Abstract:
An experimental method for evaluating the PIV measurement error and its application in optimizing PIV experiment parameters
DONG Ming-zhe, WANG Yang, JIANG Ning-tao
2005, 19(2): 79-83. doi: 10.3969/j.issn.1672-9897.2005.02.016
Abstract(102) PDF(11)
Abstract:
Flow visualization over a 2-D traveling wave wall
YANG Yi-hong, Yin Xie-zhen, LU Xi-yun
2005, 19(2): 84-90,114. doi: 10.3969/j.issn.1672-9897.2005.02.017
Abstract(114) PDF(6)
Abstract:
Study of measuring micro-bubble diameter
ZHANG Rong-sheng, ZHENG Yuan, CHENG Yun-shan
2005, 19(2): 91-95. doi: 10.3969/j.issn.1672-9897.2005.02.018
Abstract(135) PDF(4)
Abstract:
A visualization system for studying train aerodynamics
JIANG Fan, CHEN Wei-ping, TIAN Hong-qi, HE Hua
2005, 19(2): 96-102. doi: 10.3969/j.issn.1672-9897.2005.02.019
Abstract(133) PDF(2)
Abstract:
The test data visualization is very useful to study the train aerodynamics. In this paper, a new data interpolation method that combines a data field quadrilateral grid and region transformation based on the isoparametric transformation is proposed, because the data field of train aerodynamics test is the scattered data field based on curved surface. And the scanning algorithm is improved to overcome the defect of traditional algorithm, whose convergence is not ensured. In order to be able to expand the test data visualization system, the object-oriented approach is applied to the program. Finally, the test data visualization system is realized and tested, then the program is improved in practice.
Problems involved in comparison of calibration of strain gage balance in ground coordinate system and body coordinate system
WANG Jin-yin
2005, 19(2): 103-109. doi: 10.3969/j.issn.1672-9897.2005.02.020
Abstract(95) PDF(3)
Abstract:
FEM calculation and hydraulic test of NF-6 wind tunnel
XIE Ya-Jun, GUO Qi, XIAO Chun-sheng, XUE Hong-jun, XI Zhong-xiang
2005, 19(2): 110-114. doi: 10.3969/j.issn.1672-9897.2005.02.021
Abstract(109) PDF(3)
Abstract: