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Experiments and Measurements in Fluid Mechanics
1007-3124
2003 Issue 2
Investigation of the arrow wing aerodynamic performance
QIU Yuxin;LIU Gang
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page:26-31
The experimental investigation of effects of entry forms on inlet properties at low speed
WU Chaojun;YANG Wanfu;Li Zhengchu;WANG Xunnian
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page:32-36
The design and experimental investigations of supersonic free-vortex ADW
YI Shihe;HOU Zhongxi;WANG Chengrao
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page:59-62,69
Research of the vortex-shedding frequency characteristics in the annular cascade
GE Jingdong;ZHOU Hai;LU Yajun
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page:54-58
Flow visualization about a compressible shear flow
XIONG Hongliang;YUAN Ge;LI Qian;CUI Erjie
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page:74-77,83
Investigation of support interference in low speed wind tunnel oscillation tests
DU Xiqi;WANG Xuejian;ZHOU Yu
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page:37-40
Towing PIV technique and its application in a tank
ZHANG Jun; ZHAO Feng;HONG Fangwen; XU Jie
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page:93-97
The research of DPIV system and its application
WEI Runjie;SHEN Gongxin
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page:88-92
Aerodynamic experimental investigation in blade erosion of gas-solid two-phase turbine
LU Jiahua;LING Zhiguang
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page:63-69
The influences of time lag dynamic derivatives on the evaluation of the spin time history of a modified airplane
GAO Jianjun;LOU Haiye
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page:98-102
Cold flow experimental study of plug nozzle
LI Jiang1;MA Jiahuan2;PAN Wenxin2;ZHAI Manling2
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page:10-14
Study on flow characteristics and noise mechanics of impinging jet with high speed
YAO Zhaohui;HE Feng;HAN Biao;XU Hongqing
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page:84-87
Experimental investigation of the vortex characteristic over 75°/45°double delta wing
LIU Zhan;CAI Guohua
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page:41-44
Application of PIV technique in unsteady characteristics research of streak wing leading vortex
L Zhiyong;ZHU Liguo
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page:15-18
Unsteady aerodynamics in fatal accidents
WU Kaiyuan
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page:1-9
The research of civil aircraft afterbody test technique
HAO Weidong1;SI Yongchang2;LI Tong2
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page:45-48
Zonal study of flow patterns around an ogive-cylinder at subcritical Reynolds numbers
WANG Gang;DENG Xueying;WANG Yankui;CHEN Xuerui
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page:19-25,36
Wind tunnel research on statics thrust characteristics of vectoring nozzle
XU Tiejun;LI Cong;QU Fangliang
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page:49-53
A new transportation method for heavy oil by steam injector
LAI Yingxu;ZHENG Zhichu;WU Yingxiang
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page:78-83
The comparison between two deploying methods and results of folding wings for some tactical missiles
JIA Yi
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page:70-73