2005 No. 4

Display Method:
Investigation of semi-spheres on the boundary layer development over a smooth circular plate
WANG Jin-jun, DING Hai-he
2005, 19(4): 1-9. doi: 10.3969/j.issn.1672-9897.2005.04.001
Abstract(105) PDF(12)
Abstract:
The hydrogen bubble flow visualization technique was used to study the effects of small semisphere on the boundary layer transition of flow over a smooth circular plate. The experimental results indicated that the periodic hairpin vortex will shed from the semi-sphere when Rer( Reynolds number based on the radius of the semi-sphere r) was greater than 302. Due to the effect of self-induced velocity, the hairpin vortex lifted with an inclined angle. The head of the hairpin vortex moved into the higher velocity region first, so the head possessed a higher velocity than the leg part of the hairpin vortex. The hairpin vortex was strentched at the streamwise direction, which increased the streamwise vortex strength and led to much higher upward velocity of the vortex head. The continuously created strentched and self-induced processes led to the three dimensional disturbance growing quickly, so the velocity profile of the boundary layer was suffered from the temporal local strain. The strong unstable shear layer was created, which led the hairpin vortex to be broken down into turbulent spots. With the further development of the turbulent spot, the fully developed turbulent boundary layer was achieved. In addition, the strong negative fluctuation of flow velocity was observed in the transition process. The stable standing vortex was formed in the near front region of the semi-sphere, the standing vortex and the induced effect of the hairpin vortex were analyzed in detail. The disturbance created by the small semisphere was spreaded in the form of wedged shape, and the spreading angle was 5.7° for both one and three semi-spheres cases.
Numerical study on flow structure around slender with sharp nose at lower incidences
WANG Gang, LIANG Xin-gang
2005, 19(4): 10-15. doi: 10.3969/j.issn.1672-9897.2005.04.002
Abstract(115) PDF(2)
Abstract:
Investigation of waverider configuration in hypersonic wind tunnel
ZHANG Wei-min, CHEN He-wu, LI Xin-ya
2005, 19(4): 16-19. doi: 10.3969/j.issn.1672-9897.2005.04.003
Abstract(103) PDF(6)
Abstract:
Experiment research about lateral jet in hypersonic flow
XU Yun, WANG Zhi-jian, XU Xiang
2005, 19(4): 20-24. doi: 10.3969/j.issn.1672-9897.2005.04.004
Abstract(77) PDF(5)
Abstract:
Exploration of fabricating MAV foils using electro-spinning method
SI Ting, JIA Lai-bing, YIN Xie-zhen
2005, 19(4): 25-30. doi: 10.3969/j.issn.1672-9897.2005.04.005
Abstract(75) PDF(2)
Abstract:
NF-6 wind tunnel compressor and driving system
HUI Zeng-hong, HE Ming-yi
2005, 19(4): 31-35. doi: 10.3969/j.issn.1672-9897.2005.04.006
Abstract(103) PDF(6)
Abstract:
Experimental methods in a soap film tunnel
YANG Yi-hong, YIN Xie-zhen, LU Xi-yun
2005, 19(4): 36-41. doi: 10.3969/j.issn.1672-9897.2005.04.007
Abstract(114) PDF(24)
Abstract:
A preliminary study of the arc flow field for scramjet research
LIU Chu-ping, LONG Yong-sheng, BAI Han-chen, ZHANG Shao-wu, CHEN De-jiang
2005, 19(4): 42-45. doi: 10.3969/j.issn.1672-9897.2005.04.008
Abstract(129) PDF(3)
Abstract:
Investigation of roll oscillation dynamical stability derivative in rotation flow field
DU Xi-qi, BU Chen, YU Yan-ze, ZHENG Xin-jie, WANG Xue-jian
2005, 19(4): 46-48,55. doi: 10.3969/j.issn.1672-9897.2005.04.009
Abstract(89) PDF(4)
Abstract:
Experimental studies for oil-water two-phase pipeline transportation with jet pump
XU Jing-yu, WU Ying-xiang, LI Dong-hui
2005, 19(4): 49-55. doi: 10.3969/j.issn.1672-9897.2005.04.010
Abstract(93) PDF(3)
Abstract:
Investigation of tornado-type wind-powered water-pumping system
WEI Ning
2005, 19(4): 56-60. doi: 10.3969/j.issn.1672-9897.2005.04.011
Abstract(93) PDF(2)
Abstract:
The research of aerodynamic characteristics of free wing
ZHOU Yu-xiao, GU Yun-song, MING Xiao
2005, 19(4): 61-64. doi: 10.3969/j.issn.1672-9897.2005.04.012
Abstract(91) PDF(3)
Abstract:
The preparation of tracer particles with excellent scattering performance used in PIV experiment
CAI Chu-jiang, SHEN Zhi-gang, XIAO Kun, XING Yu-shan, MA Shu-lin
2005, 19(4): 65-68. doi: 10.3969/j.issn.1672-9897.2005.04.013
Abstract(117) PDF(6)
Abstract:
Experimental technique on infrared radiation in wake of blunt cone in high-enthalpy tunnel
HANG Jian, LIN Zhen-bin, GUO Da-hua, LIN Jian-min, ZENG Ming, HUANG De, GE Xue-zhen
2005, 19(4): 69-73. doi: 10.3969/j.issn.1672-9897.2005.04.014
Abstract(119) PDF(5)
Abstract:
Experimental visualization on natural gas-air mixing in engine intake
XU Sheng-li, YUE Peng-tao, LIU Kai, ZHU Zuo-jin
2005, 19(4): 74-79. doi: 10.3969/j.issn.1672-9897.2005.04.015
Abstract(122) PDF(2)
Abstract:
This paper studies the natural gas(NG)-air mixing characteristics in engine intake and the effects of injection pressure, flow speed and injector alignment. The ejection-type wind tunnel was built as a test rig. The air mass flow rate was determined by sonic throat in the duct and schlieren photograph was used to visualize the mixing flow-field. The schlieren pictures were obtained at different injection pressure, sonic throat height and injector alignment. The results show that the NG-air mixing is independent of the throttle angle less than its critical value at the specified flow speed as well as the NG injection pressure. When the values of throat height are respectively 16.4mm and 7. 1mm, the corresponding values of critical throttle angle with respective to the stream-wise direction are 51.38° and 64.87°. In contrast to wall injection, the strut injection can enhance NG-air mixing and avoid NG penetration difficulties, although the drag of strut is large. The mass flow rate of NG depends on the injection pressure and injector numbers. Upstream or the strut within the duct flow, no NG diffuses adversely.
Vortex structure and impinging tone in high-speed impinging jet
YAO Zhao-hui, HAO Peng-fei, HE Feng, XU Hong-qing
2005, 19(4): 80-84. doi: 10.3969/j.issn.1672-9897.2005.04.016
Abstract(103) PDF(2)
Abstract:
A summary on the wind tunnel test techniques for tilting-rotor aircraft
WANG Fu-xin, HUANG Ming-qi
2005, 19(4): 85-89. doi: 10.3969/j.issn.1672-9897.2005.04.017
Abstract(86) PDF(6)
Abstract: