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Study on the support interference of wire-assistant sting support at high angle of attack in low speed wind tunnel
ZHU Ming-hong, SUN Hai-sheng, JIN Ling, TANG Wei, LIU Zhi-tao
2011, 25(3): 1-5. DOI: 10.3969/j.issn.1672-9897.2011.03.001
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Experimental study of the leading edge vortex-flap of double-delta wing
LIU Tie-zhong, WANG Jin-jun, HE Hong-wei, PAN Cong
2011, 25(3): 6-9. DOI: 10.3969/j.issn.1672-9897.2011.03.002
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Investigations of grid fins geometric feature influence on drag reduction
DENG Fan, CHEN Shao-song
2011, 25(3): 10-15. DOI: 10.3969/j.issn.1672-9897.2011.03.003
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Method to eliminate the interference of model support in automotive wind tunnel
ZHANG Ying-chao, ZHANG Zhe, LI Jie
2011, 25(3): 16-19,33. DOI: 10.3969/j.issn.1672-9897.2011.03.004
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Experimental research of wide-angle diffuser performance for the intermittent wind tunnel
HUANG Zhi-long, ZHANG Guo-biao, LIU Xiao-bo, GENG Zi-hai
2011, 25(3): 20-23. DOI: 10.3969/j.issn.1672-9897.2011.03.005
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Experimental investigation on pressure field and surface flow field characteristics of large enthalpy drop aft-loading curved turbine cascade
SHI Yu-wen, WANG Zhen-feng, HAN Wan-jin
2011, 25(3): 24-29. DOI: 10.3969/j.issn.1672-9897.2011.03.006
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Hybrid laminar flow control experiment on swept wing model
DENG Shuang-guo, ERIQITAI, NIE Jun-jie
2011, 25(3): 30-33. DOI: 10.3969/j.issn.1672-9897.2011.03.007
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Experimental study on aerodynamic characteristics of a hypersonic waverider configuration
XIAO Hong, GAO Chao, DANG Yun-qing
2011, 25(3): 34-36,40. DOI: 10.3969/j.issn.1672-9897.2011.03.008
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Flutter test of rudder in sub-tran-supersonic wind tunnel using subcritical response methods
JI Chen, RAN Jin-hong, LIU Zi-qiang
2011, 25(3): 37-40. DOI: 10.3969/j.issn.1672-9897.2011.03.009
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Similarity criterion of the wind tunnel test for the post-stall maneuver
GENG Xi, SHI Zhi-wei
2011, 25(3): 41-45. DOI: 10.3969/j.issn.1672-9897.2011.03.010
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Investigation on test technique of fighters with propulsion simulation in a low speed wind tunnel
WANG Xun-nian, WU Chao-jun, CHEN Hong, LI Zhen-xu
2011, 25(3): 46-49. DOI: 10.3969/j.issn.1672-9897.2011.03.011
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Key technique for high angle of attack test of fighter aircraft in Φ3.2m low speed wind tunnel
SUN Hai-sheng, ZHU Ming-hong, HUANG Yong, LIU Zhi-tao
2011, 25(3): 50-55. DOI: 10.3969/j.issn.1672-9897.2011.03.012
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Experimental investigation on exterior orientation in vibration environment
ZHANG Zheng-yu, LUO Chuan, SUN Yan, ZHOU Gui-yu, HUANG Shi-jie
2011, 25(3): 56-59,65. DOI: 10.3969/j.issn.1672-9897.2011.03.013
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Study on the influence of ultrasonic probes on flow field and measurement performance of ultrasonic flowmeter
ZHANG Peng-yong, ZHENG Dan-dan, XU Tian-shi, ZHANG Li-xin, HU He-ming
2011, 25(3): 60-65. DOI: 10.3969/j.issn.1672-9897.2011.03.014
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Aerodynamic and structure desigh of multifunction boundary-layer wind tunnel
LIU Qing-kuan
2011, 25(3): 66-70. DOI: 10.3969/j.issn.1672-9897.2011.03.015
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Experimental technique for measuring unsteady aerodynamics of vibrating blade in turbomachinery——influence coefficient method (ICM)
YANG Hui, ZHENG Yun
2011, 25(3): 71-77. DOI: 10.3969/j.issn.1672-9897.2011.03.016
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The control system design of the high attack angle mechanism for the 8m × 6m wind tunnel
ZHOU Ping, CHANG Tian-yi, WANG Fan, JIANG Tie-deng, GUO Shou-chun, SHENG Hong, YANG Xiao-song
2011, 25(3): 78-81,96. DOI: 10.3969/j.issn.1672-9897.2011.03.017
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Research of acoustic design for aeroacoustic wind tunnel
LI Peng, TANG Geng-sheng, YU Yong-sheng, L(U) Bo
2011, 25(3): 82-86. DOI: 10.3969/j.issn.1672-9897.2011.03.018
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Five-hole flow angle probe calibration and measurement in subsonic flow
FU Cheng, PENG Qiang, LI Xian-feng, YI Xing-you
2011, 25(3): 87-90. DOI: 10.3969/j.issn.1672-9897.2011.03.019
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Selection of object plane and arrangement of knife edge for a schlieren system
LI Hua, YANG Zang-jian, WU Min, GAO Zeng-liang, ZHONG Ying-jie
2011, 25(3): 91-96. DOI: 10.3969/j.issn.1672-9897.2011.03.020
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