column
The determination of catalytic rate constant of surface materials of testing model in the shock tube
DONG Wei-zhong, LE Jia-ling, LIU Wei-xiong
2000, 14(3): 1-6. DOI: 10.3969/j.issn.1672-9897.2000.03.001
Abstract PDF
The experimental research on the interaction of a moving body with a free surface in the stratified fluid
MA Hui-yang, MA Bai-kun, ZHANG Ren-jie
2000, 14(3): 7-11,17. DOI: 10.3969/j.issn.1672-9897.2000.03.002
Abstract PDF
The measurement and diagnostics in free stream of JF-1O hydrogen oxygen detonation driven shock tunnel
LIN Zhen-bin, GUO Da-hua, ZHU Nai-yi, GE Xue-zhen, YU Xi-long, YANG Qian-suo, JIANG Nai-bo
2000, 14(3): 12-17. DOI: 10.3969/j.issn.1672-9897.2000.03.003
Abstract PDF
Analysis of unsteady aerodynamic interactions between rotor and fuselage of helicopters in forward flight
ZHA0 Jing-gen, XU Guo-hua, WANG Shi-cun
2000, 14(3): 18-24. DOI: 10.3969/j.issn.1672-9897.2000.03.004
Abstract PDF
The research of testing technique for half-model in high speed flexible adaptive wall wind tunnel
ZU0 Pei-chu, JIA0 Yu-qin, HE Jia-ju
2000, 14(3): 25-31. DOI: 10.3969/j.issn.1672-9897.2000.03.005
Abstract PDF
An experimental and numerical simulation on co-direction unsteady shock wave-boundary layer interaction
ZONG Nan, YANG Ji-ming, PAN Jian-ping, HAN Zhao-yuan
2000, 14(3): 32-36,41. DOI: 10.3969/j.issn.1672-9897.2000.03.006
Abstract PDF
Research on subsonic wall interference correction for model tests at high angle of attack
YIN Lu-ping, HE Zhong, YU Zhi-song, FAN Zhao-lin, CHEN Zuo-bin
2000, 14(3): 37-41. DOI: 10.3969/j.issn.1672-9897.2000.03.007
Abstract PDF
Experimental study on dynamic loading of shock wave on structure and equipment
TANG Jian-zeng
2000, 14(3): 42-46,51. DOI: 10.3969/j.issn.1672-9897.2000.03.008
Abstract PDF
The experiment study of wind loading on the high-strut lamp of spheriodicity lamp-bed
SONG Xian-geng, ZHA0 Lan-shui, WANG Zhao-jie, LIU Li-ping, LIN Qin-chun, DU Guang-sheng, DENG Xin-min, LIU Lian-shan
2000, 14(3): 47-51. DOI: 10.3969/j.issn.1672-9897.2000.03.009
Abstract PDF
Force measurement test technique research of flow-through model of the multi-inlet missile
WU Jun-qiang, XU Ming-fang, ZHANG Yi-feng
2000, 14(3): 52-56. DOI: 10.3969/j.issn.1672-9897.2000.03.010
Abstract PDF
Spectral measurement of nitrogen emission behind normal shock wave
YANG Qian-suo, YU Xi-long, JIANG Nai-bo, ZHU Nai-yi, LIN Zhen-bin
2000, 14(3): 57-60,65. DOI: 10.3969/j.issn.1672-9897.2000.03.011
Abstract PDF
The effects of vectored jet on leading edge vortex breakdown of 65°delta wing
WANG Jin-jun, LIU Ji-ying, XUE Qi-zhi
2000, 14(3): 61-65. DOI: 10.3969/j.issn.1672-9897.2000.03.012
Abstract PDF
The research of a new type of air cryogenic wind tunnel
LIA0 Da-xiong, TA0 yu, YU Hong-ru
2000, 14(3): 66-72. DOI: 10.3969/j.issn.1672-9897.2000.03.013
Abstract PDF
A new method to extract velocity information in PIV
YANG Yan-xiang, WANG Jian-ming
2000, 14(3): 73-78. DOI: 10.3969/j.issn.1672-9897.2000.03.014
Abstract PDF
Spectrum analysis and digital filtering to experimental data of dynamic stall test in wind tunnel
XU Yong-chang, ZHENG Shi-hua
2000, 14(3): 79-82. DOI: 10.3969/j.issn.1672-9897.2000.03.015
Abstract PDF
An empirical algorithm of aerodynamic interaction effects of rotor wake on fuselage for helicopter based on model experiments
XU Jin-fa, GAO Zheng, MEI Wei-sheng
2000, 14(3): 83-90. DOI: 10.3969/j.issn.1672-9897.2000.03.016
Abstract PDF
Design and realization of aerodynamics experimental data management system for 2.4m × 2.4m transonic wind tunnel
WANG Hong, ZHANG Jun, TANG Geng-sheng
2000, 14(3): 91-96. DOI: 10.3969/j.issn.1672-9897.2000.03.017
Abstract PDF

Submit Article

Submission Guidelines

Contact Us

Qrcode