Journal of Aerospace Power 2010 Issue 4 Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling

Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
yang wei hua ; wang mei juan ; ding you hong ; zhang jing zhou

..............page:729-734

Full elastic steady-state micro flow measurement system
zhang zuo ai ; tang hai bin ; li xin ; liu yu ; wang hai xing ; shi chen bo

..............page:847-851

Numerical study on mixing enhancement for supersonic mixing layer in dual combustor ramjet
zuo zhi hui ; chen zuo ; yu jiang fei ; liu wei dong

..............page:821-828

Experimental study of cooling effectiveness of impingement/cocurrent convection/film cooling
yang wei hua ; wang mei juan ; ding you hong ; zhang jing zhou

..............page:729-734

Dynamic response analysis of fluid-structure interaction in liquid-filled pipes of rocket feed system
wei zuo ; sun bing ; yu zi wen ; tang bo ; zhang qing song

..............page:852-856

Experiment on nitrogen-filling performance of fuel scrubbing ejector
liu xiao fang ; liu wei hua ; qian guo cheng ; zhao hong zuo

..............page:735-740

Research on the variation rules of meshing stiffness of the helical gear
bo zhong hong ; liu geng ; wu li yan

..............page:957-962

Experimental investigation of HLFC mechanism on swept wing
wang fei ; e ri qi tai ; wang qiang ; guo hui ; su pei ran

..............page:918-924

Numerical study on mixing enhancement for supersonic mixing layer in dual combustor ramjet
zuo zhi hui ; chen zuo ; yu jiang fei ; liu wei dong

..............page:821-828

Precision analysis of the flow field measured in compressor rotor by using stereoscopic particle image velocimetry
zhang zhi bo ; yu xian jun ; liu bao jie

..............page:868-876

Numerical aero-optimization method for three-dimensional compressor rotor with parameterized aerodynamic variables
he liu ; dan peng

..............page:884-890

Shallow cavity noise influencing by boundary-layer thickness at supersonic speeds
yang dang guo ; li jian qiang ; fan zhao lin ; luo xin fu ; jiang wei min

..............page:907-911

Experiment on nitrogen-filling performance of fuel scrubbing ejector
liu xiao fang ; liu wei hua ; qian guo cheng ; zhao hong zuo

..............page:735-740

Research on the variation rules of meshing stiffness of the helical gear
bo zhong hong ; liu geng ; wu li yan

..............page:957-962

Experimental investigation of HLFC mechanism on swept wing
wang fei ; e ri qi tai ; wang qiang ; guo hui ; su pei ran

..............page:918-924

Experimental investigation of spray characteristics of a double line pressure-swirl atomizer
chen jun ; ji hong hu ; zhang bao cheng

..............page:774-779

Numerical methods in simulation of annular combustor cold flow field
cai wen xiang ; zhao jian xing ; hu hao sheng ; wu xiao song

..............page:748-753

Effects of throat asymmetry on micro nozzle\'s performance
tong jun jie ; xu jin liang ; zuo ji wen

..............page:808-815

Precision analysis of the flow field measured in compressor rotor by using stereoscopic particle image velocimetry
zhang zhi bo ; yu xian jun ; liu bao jie

..............page:868-876

Shallow cavity noise influencing by boundary-layer thickness at supersonic speeds
yang dang guo ; li jian qiang ; fan zhao lin ; luo xin fu ; jiang wei min

..............page:907-911

Measurement of contact stiffness during microslip
chen zuo zuo ; ma yan hong ; li di ; hong jie

..............page:936-942

Simulation of supersonic gas-particle two-phase flow with two-fluid model
yu yong ; zhang xia ; chen wei

..............page:800-807

Experimental study on outlet temperature distribution in single vortex/lean oil trapped vortex combustor
kong xiang lei ; fan wei jun ; xing fei ; zhang rong chun ; song xuan jin

..............page:794-799

Experimental investigation of spray characteristics of a double line pressure-swirl atomizer
chen jun ; ji hong hu ; zhang bao cheng

..............page:774-779

Off-design performance study of axial flow fan in helicopter
li ming ; gao hong xia ; yu jian zu ; zhou zuo

..............page:877-883

Simulation of supersonic gas-particle two-phase flow with two-fluid model
yu yong ; zhang xia ; chen wei

..............page:800-807

Measurement of contact stiffness during microslip
chen zuo zuo ; ma yan hong ; li di ; hong jie

..............page:936-942

Effects of throat asymmetry on micro nozzle\'s performance
tong jun jie ; xu jin liang ; zuo ji wen

..............page:808-815

Film deflection measurements of a rotating film cooling model
deng hong wu ; ma ming ; luo xiang

..............page:723-728

Concurrent subspace optimization design of hypersonic cruise vehicle
che jing ; wang wen zheng ; he kai feng

..............page:912-917

Numerical methods in simulation of annular combustor cold flow field
cai wen xiang ; zhao jian xing ; hu hao sheng ; wu xiao song

..............page:748-753

Full elastic steady-state micro flow measurement system
zhang zuo ai ; tang hai bin ; li xin ; liu yu ; wang hai xing ; shi chen bo

..............page:847-851

Investigation on clocking effect of 1.5-stage transonic compressor
ren xiao dong ; gu chun wei

..............page:891-896

Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance
shen zuo xin ; liu jian jun

..............page:897-901

Off-design performance study of axial flow fan in helicopter
li ming ; gao hong xia ; yu jian zu ; zhou zuo

..............page:877-883

Denoising method for aeronautical engine turbine blade X-ray industrial CT image
fu jian ; li bin ; xiao ying chun ; jiang bai hong

..............page:857-860

Numerical investigation on pressure wave propagation speed of gas-liquid two-phase flow in pump pipeline
chen er feng ; li yan zhong ; ying zuo zuo

..............page:754-760

Dynamic response analysis of fluid-structure interaction in liquid-filled pipes of rocket feed system
wei zuo ; sun bing ; yu zi wen ; tang bo ; zhang qing song

..............page:852-856

Calibration method for microphone array on flow impedance test rig
wang li ; wang tong qing

..............page:925-929

Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance
shen zuo xin ; liu jian jun

..............page:897-901

Experimental investigation of rotating single-hole film cooling performance on suction side of a turbine blade
li guo qing ; deng hong wu ; xiao jun

..............page:780-785

Numerical aero-optimization method for three-dimensional compressor rotor with parameterized aerodynamic variables
he liu ; dan peng

..............page:884-890

Reduction of rocket engine jet noise by water injection
xu yue ; zhou xu ; zhang zhi cheng ; chen zuo ; liu li hong

..............page:816-820

Experimental study on outlet temperature distribution in single vortex/lean oil trapped vortex combustor
kong xiang lei ; fan wei jun ; xing fei ; zhang rong chun ; song xuan jin

..............page:794-799

Numerical simulation of shear dual-coaxial gas-gas injector
du zheng gang ; gao yu shan ; li mao ; jin ping ; cai guo zuo

..............page:829-834

Concurrent subspace optimization design of hypersonic cruise vehicle
che jing ; wang wen zheng ; he kai feng

..............page:912-917

Simulation experiment of the influence of elevation on performance of a rotary engine
tang ting xiao ; zhao hou liang ; chen huai hai

..............page:951-956

Numerical investigation on pressure wave propagation speed of gas-liquid two-phase flow in pump pipeline
chen er feng ; li yan zhong ; ying zuo zuo

..............page:754-760

Numerical simulation of shear dual-coaxial gas-gas injector
du zheng gang ; gao yu shan ; li mao ; jin ping ; cai guo zuo

..............page:829-834

Simulation experiment of the influence of elevation on performance of a rotary engine
tang ting xiao ; zhao hou liang ; chen huai hai

..............page:951-956

Experimental investigation of rotating single-hole film cooling performance on suction side of a turbine blade
li guo qing ; deng hong wu ; xiao jun

..............page:780-785

Denoising method for aeronautical engine turbine blade X-ray industrial CT image
fu jian ; li bin ; xiao ying chun ; jiang bai hong

..............page:857-860

Calibration method for microphone array on flow impedance test rig
wang li ; wang tong qing

..............page:925-929

Comparison of external heat transfer codes for turbine blades
qing xiong jie ; pan bing hua ; zeng jun

..............page:741-747

Investigation on clocking effect of 1.5-stage transonic compressor
ren xiao dong ; gu chun wei

..............page:891-896

Investigation on heat transfer characteristics of spiculate lamilloy internal surfaces
zhang bin ; zhu hui ren ; xu du chun

..............page:786-793

Simulation and analysis on combustion performance of hydrogen-rich/oxygen-rich gas-gas coaxial injectors
li mao ; du zheng gang ; jin ping ; cai guo zuo

..............page:835-840

Comparison of external heat transfer codes for turbine blades
qing xiong jie ; pan bing hua ; zeng jun

..............page:741-747

Reduction of rocket engine jet noise by water injection
xu yue ; zhou xu ; zhang zhi cheng ; chen zuo ; liu li hong

..............page:816-820

Numerical analysis of subsonic high-temperature-gas thermal environment simulation
yao feng ; dong su jun ; wang jun

..............page:768-773

Experimental investigation on flowrate characteristics of gaseous hydrogen/gaseous oxygen injector
gao yu shan ; du zheng gang ; li mao ; cai guo zuo

..............page:841-846

Analysis method for linear process with independent increments
fu hui min ; wu qiong

..............page:930-935

Design and application of a disturbance rejection rotor speed control method for turbo-shaft engines
zhang hai bo ; sun jian guo ; sun li guo

..............page:943-950