2009 Vol. 23, No. 1

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2009, 23(1)
Abstract(78) PDF(2)
Abstract:
Experimental research of flapping-wing propulsion for micro air vehicles
SHAO Li-min, SONG Bi-feng, SONG Wen-ping
2009, 23(1): 1-6,22. doi: 10.3969/j.issn.1672-9897.2009.01.001
Abstract(105) PDF(6)
Abstract:
PIV measurement of axial fan internal flows inside outdoor units of air-conditioner
TIAN Jie, OUYANG Hua, WU Ya-dong, DU Zhao-hui
2009, 23(1): 7-14. doi: 10.3969/j.issn.1672-9897.2009.01.002
Abstract(77) PDF(4)
Abstract:
Flow visualization of supersonic flow around a concave optical bow cap model of warhead
TIAN Li-feng, YI Shi-he, ZHAO Yu-xin, HE Lin, CHENG Zhong-yu
2009, 23(1): 15-17. doi: 10.3969/j.issn.1672-9897.2009.01.003
Abstract(96) PDF(5)
Abstract:
Experimental study of SPIV on controlling wake vortex
HUANG Shuo-qiao, SHEN Gong-xin, Robert Konrath, Carl F. v.Carmer, Kompenhans Jürgen
2009, 23(1): 18-22. doi: 10.3969/j.issn.1672-9897.2009.01.004
Abstract(98) PDF(5)
Abstract:
Investigation on bottom blockage affection on boundary layer of a plate with uniform suction in low speed wind tunnel
HUANG Zhi-xiang, CHEN Li, LI Ming, LI Jin-xue
2009, 23(1): 23-25,30. doi: 10.3969/j.issn.1672-9897.2009.01.005
Abstract(128) PDF(4)
Abstract:
Experimental analysis of vertical profiles of stream-wise velocities in flows through vegetation with PIV
HUAI Wen-xin, ZHAO Lei, LI Dan, LI Qiong
2009, 23(1): 26-30. doi: 10.3969/j.issn.1672-9897.2009.01.006
Abstract(76) PDF(4)
Abstract:
Experimental research on comprehensive measures of reducing aerodynamics effect
WANG Ying-xue, GAO Bo, SU Ke, DANG Ming-fang
2009, 23(1): 31-34. doi: 10.3969/j.issn.1672-9897.2009.01.007
Abstract(94) PDF(4)
Abstract:
Experimental investigation on the combusting jet plasmatron and diagnosis of its electron density
ZENG Xue-jun, LI Jie, WANG Zhi-jian, MA Xiao-yu, YANG Bo
2009, 23(1): 35-39. doi: 10.3969/j.issn.1672-9897.2009.01.008
Abstract(123) PDF(5)
Abstract:
A combusting jet plasmatron based on subminiature solid propellant rocket has been developed with plasma physics and aerodynamics for plasma stealth. It was obtained with Langmuir probe and its continu-um theory that the electron density distribution in longitude and cross section of jet field produced by the plas-matron. The result indicates that the jet field is a nonuniform plasma plume where contains plentiful free elec-trons and ions. The maximal electron density in the center of the jet filed is more than 4×1012 cm-3, which satisfies the primary demand on electron density for stealth plasma. The combusting jet plasmatron is a compar-atively promising technique for plasma stealth on aircrafts.
Measurement of the swirling flow field in the circular pipe with the diameter 300mm×3240mm by LDV
ZHANG Jing, SONG Jian-fei, WEI Yao-dong, SHI Ming-xian
2009, 23(1): 40-43,55. doi: 10.3969/j.issn.1672-9897.2009.01.009
Abstract(69) PDF(5)
Abstract:
Influence of electrostatic field on atomization effects for axisymmetric jet
WANG Zhao-hui, LIAO Zhen-fang, PAN Zhi-min, SHI Lei
2009, 23(1): 44-47,48. doi: 10.3969/j.issn.1672-9897.2009.01.010
Abstract(145) PDF(4)
Abstract:
An investigation of the effects of compressibility and unsteadiness on natural gas flowmeter
LIU Yan, DONG Shou-ping
2009, 23(1): 48-51. doi: 10.3969/j.issn.1672-9897.2009.01.011
Abstract(93) PDF(3)
Abstract:
Experimental research on the influence of temperature of model surface on infrared radiation and ionization
MENG Ze-jia, LIAO Guang, GUO Da-hua, LIN Zhe-nbin, LIN Jian-min
2009, 23(1): 52-55. doi: 10.3969/j.issn.1672-9897.2009.01.012
Abstract(97) PDF(4)
Abstract:
Experimental study on the aerodynamic performance of aft-loading positive-curving blade
FENG Zi-ming, HAN Wan-jin, ZHONG Jing-jun
2009, 23(1): 56-59,78. doi: 10.3969/j.issn.1672-9897.2009.01.013
Abstract(104) PDF(3)
Abstract:
Rheological research of gelatin and gelatin-PEG spinning solution
LI De-fu, MIAO Ke-yan, MU Chang-dao, YOU Qing, LIN Wei
2009, 23(1): 60-64. doi: 10.3969/j.issn.1672-9897.2009.01.014
Abstract(116) PDF(3)
Abstract:
Development of an electro-heating diaphragm rupture structure and PLIF measurement system for a shock tube
2009, 23(1): 65-69,88. doi: 10.3969/j.issn.1672-9897.2009.01.015
Abstract(77) PDF(8)
Abstract:
The development of high angle of attack test equipment in the 8m×6m low speed wind tunnel
SUN Hai-sheng, ZHANG Hui, TANG Geng-sheng, WANG Chao-qi
2009, 23(1): 70-73. doi: 10.3969/j.issn.1672-9897.2009.01.016
Abstract(104) PDF(6)
Abstract:
Design, integration and debugging on principle test system of hybrid pulse detonation engine
ZHENG Long-xi, DENG Jun-xiang, YAN Chuan-jun, LI Na, BAO Dong-mei
2009, 23(1): 74-78. doi: 10.3969/j.issn.1672-9897.2009.01.017
Abstract(92) PDF(4)
Abstract:
The control method of precise reproduction of the wing rock motion
WANG Bing, HUANG Cun-dong, MA Bao-feng, DENG Xue-ying
2009, 23(1): 79-84,104. doi: 10.3969/j.issn.1672-9897.2009.01.018
Abstract(98) PDF(3)
Abstract:
Identification of aerodynamic derivatives for bridge sections by LSCE method
WANG Wei-hua, YANG Zhuan-yun, LIU Hui
2009, 23(1): 85-88. doi: 10.3969/j.issn.1672-9897.2009.01.019
Abstract(83) PDF(3)
Abstract:
A new type of hot-wire/film anemometer
SHENG Sen-zhi, ZHUANG Yong-ji, LIU Zong-yan
2009, 23(1): 89-93. doi: 10.3969/j.issn.1672-9897.2009.01.020
Abstract(111) PDF(4)
Abstract:
The research of intelligent wireless sensor network (WSN) and wireless measurement technology for wind tunnel
HAN Jie, TANG Xiao-shan, ZHOU Ping, LI Nan
2009, 23(1): 94-98. doi: 10.3969/j.issn.1672-9897.2009.01.021
Abstract(88) PDF(3)
Abstract:

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