Journal of Aerospace Power 2012 Issue 6 Effect of film cooling hole entrance position on film cooling characters in the cross-flow passage with ribs

Effect of film cooling hole entrance position on film cooling characters in the cross-flow passage with ribs
LI Chun-lin;ZHU Hui-ren;BAI Jiang-tao; DU Xiao-qin;ZHOU Lei-sheng

..............page:1340-1346

Three-dimensional numerical simulation of hybrid rocket motor operation process
LI Xin-tian;TIAN Hui;ZENG Peng;CAI Guo-biao

..............page:1398-1404

ji yu bing xing duo mu biao yi chuan suan fa da han dao fen kai shi pai qi xi tong qi dong you hua she ji
xiong jian wang xin yue shi yong qiang zuo zi guang

..............page:1384-1390

Tooth meshing contact analysis for bevel gears by face hobbing method based on arc blade profile
NIE Shao-wu1;DENG Xiao-zhong2;LI Tian-xing1;ZHANG Hua2;DENG Jing1

..............page:1424-1431

Characterization of nozzle thermal and ablation response in dual-pulse solid rocket motors
ZHANG Xiao-guang;LIU Yu;WANG Chang-hui

..............page:1391-1397

Influence of entropy layer on aerodynamics parameters for hypersonic 2-D blunt wedge
CHENG Xing-hua;YANG Tao;CHANG Zhong-dong

..............page:1362-1367

ji yu dian zi shu dian li de ci liu ti li xue jin qi dao liu dong kong zhi shu zhi mo ni
zhang xiang hong wu zuo zhao wang jiang feng

..............page:1375-1383

Design and numerical investigation of hypersonic inward turning inlet with water-drop like shape intake
LI Yong-zhou;Zhang Kun-yuan;NAN Xiang-jun;ZHANG Lin

..............page:1355-1361

ji yu yuan hu dao kuo de duan mian gun qie zhui chi lun nie he jie chu fen xi
nie shao wu deng xiao zhong li tian xing zhang hua deng jing

..............page:1424-1431

Structure optimization design for blisk based on ANSYS
LU Shan;LU Feng-jie

..............page:1218-1224

ji zai zhi dan xi tong zhong kong xian wei mo fen li te xing
feng shi yu lu ji liu wei hua jiang jun chang liu su yan

..............page:1332-1339

ge xiang yi xing duo zhou jin si ying li ying bian fen xi fang fa yan jiu ji ying yong
wang jing ke yang xiao guang

..............page:1230-1237

da xing shui lu liang qi fei ji yi xing you hua she ji
qin he jun zeng you bing

..............page:1368-1374

Aerodynamic optimization design of high bypass ratio separate-flow exhaust system based on parallel multi-objective genetic algorithm
XIONG Jian;WANG Xin-yue;SHI Yong-qiang;YAN Zi-guang

..............page:1384-1390

Experimental investigation on cold flow characteristics of afterburner with cavity/strut hybrid flameholders
QIN Wei-lin;HE Xiao-min;JIN Yi;JIANG Bo

..............page:1347-1354

li xin ya qi ji zi xun huan yu xuan pen qi ji xia chu li de she ji he yan zheng
kang jian xiong du qiang huang guo ping zhu jun qiang wen dian zhong

..............page:1297-1302

fault diagnosis and isolation of the componentand sensor for aircraft engine
QIU Xiao-jie;HUANG Jin-quan;LU Feng;LIU Nan

..............page:1432-1440

yi zhong cao dao shi chu li ji xia de zhun ding chang liu dong mo xing kua sheng zhuan zi chu li ji xia de you hua she ji
fan lin ning fang fei liu huo xing

..............page:1278-1287

Implicit coupled solution of the combustion chamber with the spray
ZHENG Qun;LI Yi-jin;SUN Lan-xin

..............page:1320-1325

wo lun pan / zheng ti jie gou you hua she ji fang fa
tao ye lu shan

..............page:1249-1354

Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor
KANG Jian-xiong1;2;DU Qiang2;HUANG Guo-ping1;ZHU Jun-qiang2;WEN Dian-zhong3

..............page:1297-1302

ji yu duo ceng you hua ce lue de wo lun pan ye she ji yan jiu
wang rong qiao jia zhi gang yang jun jie hu dian yin fan jiang shen xiu li

..............page:1201-1209

Opportunities and challenges of MEMS technologyin the environment of intelligent aero-engines
YAN Xiao-jun1;ZHANG Kai1;WU Xiao-ming2

..............page:1210-1217

li xin ya qi ji guan shi kuo ya qi she ji yu ji suan fen xi
wang bo yan ming

..............page:1303-1311

mems ji shu zai zhi neng hang kong fa dong ji zhong de ying yong yan jiu xian zhuang ji qian jing
zuo xiao jun zhang zuo wu xiao ming

..............page:1210-1217

zhou liu wo lun ji yuan ji dong ye chou du te xing de shu zhi yan jiu
yang jie qiao wei yang hou wei tao wei zuo jun

..............page:1288-1296

mou xing fei ji fa dong ji duan cang fang bing xi tong she ji ji suan
zhu yong feng fang yu feng feng wen chun

..............page:1326-1331

ao qiang zhu wo yu zhi ban wen yan zu he jia li ran shao shi mo xing leng tai liu chang shi yan
qin wei lin he xiao min jin yi jiang bo

..............page:1347-1354

Design and numerical simulation of pipe diffuser in centrifugal compressor
WANG BO;YAN Ming

..............page:1303-1311

Fault diagnostics system for helicopter main gearbox using wavelet neural network
LIU Li-sheng1;2;YANG Yu-hang2

..............page:1255-1260

yin shi zuo he qiu jie ran shao shi nei pen wu liang xiang liu chang
zheng qun li yi jin sun lan zuo

..............page:1320-1325

Separation performance of hollow fiber membrane for on-board inerting gas generating system
FENG Shi-yu1;LU Ji1;LIU Wei-hua1;JIANG Jun-chang2;LIU Su-yan2

..............page:1332-1339

Static characterization of bump-type gas foil bearing:intergration of top foil 2-D thick plate model
LIU Zhan-sheng;XU Fang-cheng;ZHANG Guang-hui;CAO Zhi-xuan

..............page:1405-1415

Quasi-steady flow model of slot-type casing treatments Ⅰ:modeling method and validation
NING Fang-fei;FAN Lin

..............page:1261-1269

Method of stability region determination for planetary gear train’s parameters based on nonlinear vibration model
LI Tong-jie1;2;ZHU Ru-peng1;BAO He-yun1;XIANG Chang-le3;LIU Hui3

..............page:1416-1423

Experimental evaluation of steady-state effect of inlet radial total pressure distortion under multistage environment
XIANG Hong-hui1;2;HOU Min-jie1;GE Ning2; WU Sen-lin1;YANG Rong-fei2

..............page:1270-1277

Adaptive incremental Kalman filter method
FU Hui-min;WU Yun-zhang;LOU Tai-shan

..............page:1225-1229

Implicit algorithm for viscous compressible flow on unstructured grids
WANG Jing-yu1;GE Ning1;SHENG Chun-hua2

..............page:1312-1319

Numerical study on the rotor solidity characteristics of axial turbine element stages
YANG Jie;QIAO Wei-yang;HOU Wei-tao;WEI Zuo-jun

..............page:1288-1296

Experimental and prediction study for bearing capacityof inflatable wing
WANG Zhi-fei;WANG Hua;WANG Wei;JIA Qin-ping

..............page:1243-1248

kang hun die shi pin yu rong he suan fa ji zai ye pian xiang ying fen xi zhong de ying yong
liu ya lin shang guan bo xu zi li

..............page:1238-1242

dai lei heng liu tong dao zhong qi mo kong wei zhi dui qi mo leng que te xing de ying xiang
li chun lin zhu hui ren bai jiang tao du xiao qin zhou lei sheng

..............page:1340-1346

shuang mai chong gu ti fa dong ji pen guan chuan re shao shi te xing
zhang xiao guang liu yu wang chang hui

..............page:1391-1397

Numerical simulation for magnetohydrodynamic inlets control using electron beam ionization
ZHANG Xiang-hong;WU Yi-zhao;WANG Jiang-feng

..............page:1375-1383

Study on disk and blade design based on multi-layeroptimization strategy
WANG Rong-qiao;JIA Zhi-gang;YANG Jun-jie;HU Dian-yin; FAN Jiang;SHEN Xiu-li

..............page:1201-1209

zi shi ying zeng liang kalman lv bo fang fa
fu hui min wu yun zhang lou tai shan

..............page:1225-1229

ji yu xiao bo shen jing wang luo de zhi sheng ji zhu jian su qi gu zhang zhen duan xi tong
liu li sheng yang yu hang

..............page:1255-1260

zuo ceng dui gao chao sheng su er wei dun xie qi dong can shu de ying xiang
cheng xing hua yang tao chang zhong dong

..............page:1362-1367

Anti-aliasing alternating frequency/time domain method and its application in response analysis of blade systems
LIU Ya-lin1;SHANGGUAN Bo1;XU Zi-li2

..............page:1238-1242

duo ji huan jing xia jing xiang zong ya ji bian ying xiang xiao ying de shi yan ping jia
xiang hong hui hou min jie ge ning wu sen lin yang rong fei

..............page:1270-1277

rou xing ji yi cheng zai neng li de shi yan yu yu ce
wang zhi fei wang hua wang wei jia qing ping

..............page:1243-1248

yi zhong cao dao shi chu li ji xia de zhun ding chang liu dong mo xing jian mo fang fa ji yan zheng
ning fang fei fan lin

..............page:1261-1269

xing xing chi lun fei xian xing zhen dong xi tong can shu wen ding yu de ji suan fang fa
li tong jie zhu ru peng bao he yun xiang chang le liu hui

..............page:1416-1423

lei shui di jin kou gao chao sheng su nei shou suo jin qi dao she ji ji shu zhi yan jiu
li yong zhou zhang yuan nan xiang jun zhang lin

..............page:1355-1361

ji yu ansys de zheng ti ye pan jie gou you hua she ji
lu shan lu feng jie

..............page:1218-1224

fei jie gou wang ge xia ke ya suo zuo xing liu ti de yin shi suan fa
wang jing yu ge ning sheng chun-hua

..............page:1312-1319

Quasi-steady flow model of slot-type casing treatments Ⅱ:design optimization of casing treatment for a transonic rotor
FAN Lin;NING Fang-fei;LIU huo-xing

..............page:1278-1287

gu ye huo jian fa dong ji gong zuo guo cheng san wei shu zhi fang zhen
li xin tian tian hui zeng peng cai guo zuo

..............page:1398-1404

ji yu er wei hou ban mo xing de bo bo pian zhou cheng jing te xing
liu zhan sheng xu fang cheng zhang guang hui cao zhi xuan

..............page:1405-1415

Optimum airfoil design on an heavy amphibious aircraft
QIN He-jun;ZENG You-bing

..............page:1368-1374

Method of structural optimization design for turbine disk/tenon
TAO Ye;LU Shan

..............page:1249-1254

flult diagnosis and isolation of the component and sensor for aircraft engine
qiu xiao-jie huang jin-quan lu feng liu nan

..............page:1432-1440

Study and application on anisotropic multiaxial approximate stressand strain analysis method
WANG Jing-ke;YANG Xiao-guang

..............page:1230-1237

Design and calculation of aircraft nacelle anti-icing system
ZHU Yong-feng1;3;FANG Yu-feng2;FENG Wen-chun3

..............page:1326-1331