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Impulse combustion wind tunnel and its application in rocket and scramjet research
LE Jia-ling, LIU Wei-xiong, HE Wei, TAN Yu, BAI Han-chen
2005, 19(1): 1-10. DOI: 10.3969/j.issn.1672-9897.2005.01.001
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Unsteadiness of shock-wave/boundary-layer interactions induced by unswept and sweptback ramps
HU Cheng-hang, JIANG Wei-min, HUANG Xu-hui, ZHOU Wen-jun, XU Lai-wu
2005, 19(1): 11-16. DOI: 10.3969/j.issn.1672-9897.2005.01.002
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Influence of nonlinear gas oscillations on rectangular wings
SUN Jian-hong, LI Qi-chang, LIU Jun-zhi
2005, 19(1): 17-21,34. DOI: 10.3969/j.issn.1672-9897.2005.01.003
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Instantaneous investigation of gas-solid two-phase free jet flow
YANG Ren-gang, ZHANG Dong-dong, HE Feng, XU Hong-qing
2005, 19(1): 22-25. DOI: 10.3969/j.issn.1672-9897.2005.01.004
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Experimental study on differential-resistance model in multiphase flow metering
LIN Jun, DONG Shou-ping, Huang Hui
2005, 19(1): 26-30. DOI: 10.3969/j.issn.1672-9897.2005.01.005
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Investigation of longitudinal damping derivative of aircraft by direct measurement tests
BU Chen, DU Xi-qi, WANG Xue-jian
2005, 19(1): 31-34. DOI: 10.3969/j.issn.1672-9897.2005.01.006
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An investigation on the effect of the acoustic excitation on flow asymmetry over a slender revolution body at high angles of attack in compressible flows
FAN Zhao-Lin, WANG Yuan-Jing, HOU Yue-long, HE Zhong
2005, 19(1): 35-39,51. DOI: 10.3969/j.issn.1672-9897.2005.01.007
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Experimental research on the off-design performance of the axial rotors with forward-skewed blades
YANG Bo, LIU Fu-bin, ZHONG Fang-yuan, WANG Tong, GU Chuan-gang
2005, 19(1): 40-46. DOI: 10.3969/j.issn.1672-9897.2005.01.008
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Identification of aerodynamic derivatives for bridge sections by forced oscillation method
WANG Wei-hua, LI Ming-shui, CHEN Xin
2005, 19(1): 47-51. DOI: 10.3969/j.issn.1672-9897.2005.01.009
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Experimental study on cavitation inception of nozzles with different geometries
YI Can, LI Gen-sheng, ZHANG Ding-guo
2005, 19(1): 52-55,60. DOI: 10.3969/j.issn.1672-9897.2005.01.010
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Experimental research on quick speed-changing device for low speed wind tunnel
LIU Zheng-chong, LIU Qin, ZHANG Guo-biao
2005, 19(1): 56-60. DOI: 10.3969/j.issn.1672-9897.2005.01.011
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Research on the Mach number control system in NF-6 wind tunnel
HUI Zeng-hong, HE Ming-yi, ZHU Zhao-xia
2005, 19(1): 61-65. DOI: 10.3969/j.issn.1672-9897.2005.01.012
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Development of the balance for crew escape system at large angles of attack and sideslip angles
CHEN De-hua, LI Xiao-hua, PENG Yun
2005, 19(1): 66-70,78. DOI: 10.3969/j.issn.1672-9897.2005.01.013
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The development of the interference force measurement balance for sub-missile
WANG Yu-hua, ZHAO Zhong-liang
2005, 19(1): 71-74. DOI: 10.3969/j.issn.1672-9897.2005.01.014
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The research of the steady-state heat-flux measurement technique for aerothermodynamic experiment
CHEN De-jiang, WANG Guo-lin, QU Yang, WANG Zhang-jian, WU Li-heng
2005, 19(1): 75-78. DOI: 10.3969/j.issn.1672-9897.2005.01.015
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Research on Mach number control compensation decoupling for wind tunnel
ZHAO Shu-jun, CHI Yan, SHI Hong-chang, TANG Xiao-dong
2005, 19(1): 79-82,108. DOI: 10.3969/j.issn.1672-9897.2005.01.016
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Investigation on the characteristics and structures of unsteady flow field near the Zero-mass flux jet with PIV
GU Yun-song, MING Xiao
2005, 19(1): 83-86. DOI: 10.3969/j.issn.1672-9897.2005.01.017
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Experimental study on rectangular turbulent impinging jet flow field by PIV technique
CHEN Qing-guang, XU Zhong, WU Yu-lin, ZHANG Yong-jian, ZHANG Yong-chao
2005, 19(1): 87-93. DOI: 10.3969/j.issn.1672-9897.2005.01.018
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Separation technique for oil-gas multi-phase flow transportation in submarine pipeline
ZHENG Zhi-chu, ZHOU Yong, GUO Jun, ZHANG Jun, TANG Chi
2005, 19(1): 94-98. DOI: 10.3969/j.issn.1672-9897.2005.01.019
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Fuzzy logic modeling of nonlinear unsteady aerodynamics
LIU Zhi-tao, SUN Hai-sheng, JIANG Yu-biao, JIANG Feng
2005, 19(1): 99-103. DOI: 10.3969/j.issn.1672-9897.2005.01.020
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Optimum aerodynamic design of transonic airfoils based on response surface methodology
XIONG Jun-tao, QIAO Zhi-de
2005, 19(1): 104-108. DOI: 10.3969/j.issn.1672-9897.2005.01.021
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Investigation of improving the lateral static stability for the aircraft applied to high-subsonic flow and high angle of attack
CHEN Bin
2005, 19(1): 109-112. DOI: 10.3969/j.issn.1672-9897.2005.01.022
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