1672-9897
2010 Issue 3
Study on the swept wing crossflow stationary wave and its harmonics
li yue li ; li dong ; yang yong ; zuo sui han
li yue li ; li dong ; yang yong ; zuo sui han
..............page:25-28
Experimental study on vortex-control technology of canard-spanwise synthetic jet actuators on close-coupled canard configuration
cao shuo ; liu pei qing ; fan wen bo
cao shuo ; liu pei qing ; fan wen bo
..............page:1-5
Study on quasi-two-dimensional submerged vertical over-expanded supersonic jets
guo qiang ; shi hong hui ; wang chao ; jia hui xia
guo qiang ; shi hong hui ; wang chao ; jia hui xia
..............page:6-11,18
Investigation on calibration method of hot-wire anemometer in high pressure reciprocating flow
lun li yong ; chen hou lei ; cai jing hui
lun li yong ; chen hou lei ; cai jing hui
..............page:87-91
Study of interactions between stream-wise vortex and secondary vortices in turbine cascade
wang peng ; zou zheng ping ; zuo lei ; liu huo xing ; ye jian
wang peng ; zou zheng ping ; zuo lei ; liu huo xing ; ye jian
..............page:42-49
Experimental investigation on flow characteristics during double limit cycle oscillation induced by forebody vortex
rong zhen ; deng xue ying ; wang bing ; ma bao feng
rong zhen ; deng xue ying ; wang bing ; ma bao feng
..............page:19-24
Experimental studies of controlling hydrofoil stall by electromagnetic force
liu peng ; li yan xia ; zhou ben mou
liu peng ; li yan xia ; zhou ben mou
..............page:29-33
Experimental study on the influence of bubbles on dynamic characteristics of valve-less micropump
jiang dan ; li song jing ; yang ping
jiang dan ; li song jing ; yang ping
..............page:34-38,62
Experimental investigation of split-rudder deflection on aerodynamic performance of tailless flying-wing aircraft
zhang zi jun ; li jun ; li tian ; wang jin jun
zhang zi jun ; li jun ; li tian ; wang jin jun
..............page:63-66
A test technique for multi-boby interference and separation in hypersonic wind tunnel
wu ji fei ; wang yuan jing ; luo xin fu ; qian feng xue
wu ji fei ; wang yuan jing ; luo xin fu ; qian feng xue
..............page:99-102
Effects of initial perturbations on Rayleigh-Taylor instability growth at gas-liquid interface
huang wen bin ; zou li yong ; liu jin hong ; tan duo wang ; zhang guang
huang wen bin ; zou li yong ; liu jin hong ; tan duo wang ; zhang guang
..............page:39-41,66
Research on features of fluctuating wind pressure on large hyperbolic cooling tower: features of non-Gaussian
ke shi tang ; ge yao jun ; zhao lin
ke shi tang ; ge yao jun ; zhao lin
..............page:12-18
In-flight test measurement of flap pressure distribution for aerotransport
cao hu cheng ; zhou zhan ting ; li shao peng
cao hu cheng ; zhou zhan ting ; li shao peng
..............page:96-98
Effect of elastic deformation on aerodynamic characteristics of the flexible airship
chen hua ; zhang zhao ming
chen hua ; zhang zhao ming
..............page:59-62
Investigation about drag reduction characteristic of riblets surface on vehicle model in water tunnel
huang qiao gao ; pan guang ; hu hai bao ; liu zhan yi
huang qiao gao ; pan guang ; hu hai bao ; liu zhan yi
..............page:50-53
Research on automatic variable-angle system of the buried motivator
dong guo qing ; li qiang ; li zhou fu ; xu long jin ; liu xi he
dong guo qing ; li qiang ; li zhou fu ; xu long jin ; liu xi he
..............page:73-76,98
..............page:封4
Investigation on component loss of icing wind tunnel
liu wei hong ; peng qiang ; fu cheng ; huang wei min
liu wei hong ; peng qiang ; fu cheng ; huang wei min
..............page:92-95
Experiments of single phase flow characteristics for swirl microchannel under overload acceleration
yang zuo ; yu jian zu ; gao hong xia ; xie yong qi ; xi you min
yang zuo ; yu jian zu ; gao hong xia ; xie yong qi ; xi you min
..............page:67-72
Spot extraction of nano-particles in MPT method
wang xu wei ; li zhan hua
wang xu wei ; li zhan hua
..............page:77-80
Application of pressure sensitive paint on aerodynamic load measurement of delta wing model in supersonic wind tunnel
xiang xing ju ; lang wei dong ; xiong hong liang
xiang xing ju ; lang wei dong ; xiong hong liang
..............page:81-86
Investigation of HLFC on swept wing based on sublimation technique
wang fei ; e ri qi tai ; wang qiang ; guo hui ; su pei ran
wang fei ; e ri qi tai ; wang qiang ; guo hui ; su pei ran
..............page:54-58