Journal of Aerospace Power 2012 Issue 10 Rectangular tooth straight through labyrinth seal analytical model

Rectangular tooth straight through labyrinth seal analytical model
WU Hong;LI Peng;TAO Zhi

..............page:2180-2187

Heat transfer in direct transfer pre-swirl rotor-stator system
XU Guo-qiang;ZHAO Xi;LUO Xiang;CAI Xu;YU Hong-peng

..............page:2161-2168

Frame plate and flame holder integration design and capability analysis
LI Feng1;CHENG Ming1;2;GUO Rui-qing1;SHANG Shou-tang1;2; TANG Zheng-fu1;2;LI LONG-xian1

..............page:2169-2174

Numerical simulation of flow and heat transfer performances in a direct transfer pre-swirl system
LUO Xiang;FENG Ye;XU Guo-qiang;ZHAO Xi;ZHAO Nan

..............page:2188-2193

Full status two phase turbulent combustion model
WANG Fang;HUANG Yong

..............page:2200-2204

Experiment on performance of annular interstage turbine burner
SONG Shuang-wen;HU Hao-sheng;WANG Mei-juan; CHEN Jian;WANG Lu-feng

..............page:2175-2179

Rotating long orifices with radiused inlets analytical model
LI Peng;WU Hong;TAO Zhi

..............page:2205-2213

Relationship of failure of fuel nozzle seal spring and engine smoking failure
XU Yong-gang1;2;WANG Qiang1 Company Limited; Aviation Industry Corporation of China;Xi’an 710021;China)

..............page:2194-2199

Experiment on combustion characteristics of novel variable geometry flame-holder
LIU Yang;JIN Jie;WANG Hui-ru;YANG Mao-lin

..............page:2214-2221

Effects of liner pressure loss on combustor ignition performances
XUE Xin;LIN Yu-zhen;ZHANG Chi;XU Quan-hong;DU Jiang-yi

..............page:2229-2235

Design and simulation of electronic micro multiple fixed-volume fuel injection system
ZHANG Qi1;YANG Kai1;XU Guo-qiang2;DU Fa-rong2

..............page:2243-2248

Effect of serrated cut at trailing edge on performance of lobed mixer in forced mixing exhaust system
DING Yu-lin1;LIU You-hong1;XIE Yi1;SHAO Wan-ren2;WU Fei2

..............page:2236-2242

Vaporization and spray characteristics of vaporizer
RUAN Chang-long1;XU Quan-hong1;SUN Dong-wen2; ZHANG Chi1;LIN Yu-zhen1 Corporation Limited; Aviation Industry Corporation of China;Harbin 150066;China)

..............page:2249-2253

Application of similitude theory in modified design of a fan
JI Guo-feng1;WANG Hua-qing1;GUI Xing-min2;DENG Shao-chun1

..............page:2254-2261

Method of measuring 3-D unsteady flow at exits of transonic compressor rotor passages using a two-hole tip-wedge pressure probe
LI Jing-yang 1;2;MA Hong-wei1;HE Xiang1

..............page:2262-2268

Analysis of blade vibration response induced by rotating stall in axial compressor
ZHANG Ming-ming;HOU An-ping;LI Jian-xiong;YAO Juan;CHEN Ying-xiu

..............page:2269-2277

Analysis of matching characteristic of transonic tandem stator airfoil and its optimization
TAO Yuan;YU Xian-jun;LIU Bao-jie

..............page:2278-2286

Influences of several parameters on aerodynamic performance of micro-radial turbine
BIAN Lei1;YAN Ze-Xiang2;ZOU Zheng-ping1

..............page:2287-2296

Effect of axial spacing on aerodynamic excitation of rotor blade
XIAO Da-qi;ZHENG Yun;YANG Hui

..............page:2307-2313

Experiment of flow characteristics of direct transfer pre-swirl system
CAI Xu;XU Guo-qiang;LUO Xiang;ZHAO Xi;LI Ye

..............page:2222-2228

Structure optimization method of radial inflow impeller based on design of experiment and support vector machine
MI Dong1;2;YIN Ze-yong1;2;QIAN Zheng-ming2; ZHANG Zhi-yi2;FENG Li-yong2

..............page:2336-2341

Numerical investigation of effect of radial vane diffuser fillet on performance of centrifugal compressor
TANG Hui;NING Fang-fei

..............page:2297-2306

Strength considerations for concept design of turbine blade
YANG Xiao-guang1;HU Xiao-an1;SHI Duo-qi1;WANG Jing-ke2;HUANG-Jia1

..............page:2314-2320

Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle
SHAO Wan-ren1;2

..............page:2356-2363

Transient response of startup process for fluidic control vector nozzle
WANG Meng-jie;Eriqitai;WANG Qiang

..............page:2364-2370

Numerical simulation of infrared radiation characteristic of exhaust system using Tam-Ganesan turbulence model
LI Xi-xi;Eriqitai

..............page:2384-2389

Application of new boundary method in Cartesian-mesh
HAN Yu-qi;JIANG Li-jun;ZHANG Chang-xian;GAO Ge

..............page:2371-2377

Simulation of three-dimensional magnetohydrodynamic enhanced scramjet
ZHENG Xiao-mei;YANG Xing-yu

..............page:2390-2400

Life prediction method based on characteristic of cyclic stress
WEI Da-sheng1;WANG Yan-rong1;WANG Xiang-ping2;WANG Hong-bin2

..............page:2342-2347

Aerodynamic characteristics of sonic injection through diamond-shaped orifices in supersonic flow field
ZHANG Ding-wu;WANG Qiang;HU Hai-yang

..............page:2378-2383

Analysis of elastoplastic response in FGH97 notched specimens based on viscoplastic constitutive model
YUAN Shan-hu;WEI Da-sheng;WANG Yan-rong

..............page:2348-2355

Dynamic response of aero-engine rotor system with bearing misalignment
ZHANG Zhen-bo1;2;MA Yan-hong2;LI Jun2;HONG Jie2

..............page:2321-2328

Internal structure of three-dimensional hollow blade with equal strength
LI Lin;XUE Zheng

..............page:2329-2335