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Investigation and application of two-component pressure sensitive paint technique
DENG Xue-ying, ZHANG Yong-cun, CHENG Hou-mei, MA Xiao-guang, CHEN Xue-yuan, YAN Li, ZHAO Wen-tao, SHANG Jin-kui, GUO Fa-chun, CHEN Liu-sheng
2010, 28(5): 485-489.
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Study on in-cylinder swirl flow of a four-valve gasoline engine with swirl control valves on intake manifolds
LI Ming, LIU De-xin
2010, 28(5): 490-494.
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Experimental investigation of cross-flow instability in swept-wing boundary layers
ZUO Sui-han, YANG Yong, LI Dong, LI Yue-li
2010, 28(5): 495-502.
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Propeller wake analysis by means of PIV in large water tunnel
LI Guang-nian, ZHANG Jun, ZHANG Guo-ping, LU Lin-zhang
2010, 28(5): 503-508.
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Aerodynamic design method based on N-S equations and discrete adjoint approach
ZUO Ying-tao, GAO Zheng-hong, HE Jun
2010, 28(5): 509-512,.
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Preliminary study on correlative parameters of extrapolation-to-flight of aerodynamic heating from wind tunnels
LIAO Jun-bi, LI Ming, ZEN Xue-jun, ZHU Zhi-wei, ZHANG Kou-li
2010, 28(5): 513-517.
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Effects of segmented Gurney flaps on the aerodynamics of a target drone model
ZHAO Yuan-li, ZUO Lin-xuan, YU Dong-sheng, WANG Jin-jun
2010, 28(5): 518-524.
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An artificial transition technique applied to wing rock induced by forebody vortex
WANG Bing, DENG Xue-ying, MA Bao-feng, RONG Zhen
2010, 28(5): 525-535.
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Numerical investigation of a flutter exciting system based on overset grids
XU He-yong, YE Zheng-yin, Huo Xing-li
2010, 28(5): 536-539,.
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A feature-based data mining method for fluid dynamics
ZHOU Di-bin, XIE Li-jun, ZHANG Shuai, ZHANG Ji-fa, ZHENG Yao
2010, 28(5): 540-546.
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A method of wind velocity distribution above the sea surface in near-shore waters
SONG Zhi-yao, NI Zhi-hui, WU Li-chun
2010, 28(5): 547-552.
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Numerical investigation of lateral jets in supersonic cross-flows
CAI Jin-sheng, LIU Qiu-hong
2010, 28(5): 553-558.
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Aerodynamic characteristics and flow mechanism of the configuration with variable forward-swept wing
LIU Wen-fa, WANG Xu, LIU Xiong
2010, 28(5): 559-564.
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The aerodynamic design and experimental research on high-speed axial-flow fan applied in the axial-flow pneumatic extinguisher
YU Guo-sheng, QIN Rui-hong, CHU Shuang-lei
2010, 28(5): 565-570,.
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Analysis for the effects of diesel engine helical inlet track's structure parameters on airway performances
BI Yu-hua, He Chang-ming, LEI Ji-lin, SHEN Li-zhong
2010, 28(5): 571-575.
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Experiments for reducing a flow field impacts on the light transmition by a guide plate
FU Song, CHEN Zhi-qiang, GUO Long-de, XIE Wei-ming
2010, 28(5): 576-581.
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Numerical simulation of vortex-induced vibration of three cylinders subjected to a cross flow in equilateral arrangement
XU Feng, OU Jin-ping
2010, 28(5): 582-590.
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The method of heat flux calculation base on integral method
CHEN Si-yuan, JIANG Gui-qing, ZHANG Liang
2010, 28(5): 591-595.
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Study on eulerian method for icing collection efficiency computation and its application
YI Xian, WANG Kai-chun, GUI Ye-wei, ZHU Guo-lin
2010, 28(5): 596-601,.
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Investigation to disposition scheme of 2DPIV field of view
DONG Chao, DENG Xue-ying, WANG Yan-kui, ZHANG Jie
2010, 28(5): 602-608.
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Study of aero-optical aberration measuring method based on BOS
ZHANG Hong-chao, ZHAO Yu-xin, YANG Tao
2010, 28(5): 609-612.
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Research status of TBCC inlet and its key technologies
GUO Rong-wei, LI Bo, ZHANG Hua-jun
2010, 28(5): 613-620.
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