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Journal of Aerospace Power
1000-8055
2011 Issue 6
Impact of geometry parameters on the thrust and infrared radiation characteristics of two-dimensional ejector nozzle
LIU Fu-cheng;JI Hong-hu;LIN Lan-zhi;HUANG Wei;LIU Chang-chun;SI Ren
..............page:1244-1250
Numerical simulation of swirling flow with different turbulent models
FENG Xi-ping;ZHAO Sheng-hai;LI Jin-xian;CAO Qi
..............page:1209-1214
Natural vibration analysis of bearingless rotor blades
LI Xue-chang;LI Shu
..............page:1237-1243
Study on meshing characteristics of helipoid gears with surface modification
SU Jin-zhan;FANG Zong-de;WANG Zu-bing
..............page:1436-1440
Research on combustion efficiency of cavity-type ramjet
TAN Jian-guo;HUANG Guo-qing;PAN Yu;WANG Zhen-guo
..............page:1415-1419
Progress of investigation on combustion instability of solid rocket motors
WANG Ning-fei;ZHANG Qiao;LI Jun-wei;SU Wan-xing
..............page:1405-1414
Optimization and design of an impeller assist heart pump device
YANG Xiao-chen1;2;ZHANG Yan3;GUI Xing-min1;2
..............page:1370-1376
Secondary flow analysis for non-axisymmetric endwall on the high-load compressor cascade
WU Ji-chang1;2;LU Xin-gen1;ZHU Jun-qiang1
..............page:1362-1369
Geared turbofan engine transient modeling research based on CMF method
TONG Wan-jun;TANG Shi-jian
..............page:1377-1383
Data processing of blade’s transient heat transfer experiment in short duration wind tunnel
ZHU Hui-ren;CHENG Wen-juan;LI Hong-cai
..............page:1301-1309
Low cycle fatigue life experiment of sheet metal with coldworking hole
YANG Xing-yu;WANG Yu-ya;DONG Li-wei;MENG Xiang-ming;TUO Wei
..............page:1257-1265
Application of recycling/rescaling method in hybrid LES/RANS simulation method
CHEN Ti;LIU Wei-dong;FAN Xiao-qiang;SUN Ming-bo
..............page:1215-1222
Support vector machine complex method for multi-dimensional sensor calibration
MA Ying-kun;ZHANG Xi-nong
..............page:1274-1281
Integral inference method for da/dN-ΔK and P-da/dN-ΔK curves
FU Hui-min;WU Qiong
..............page:1251-1256
Structure design and shape optimization in arc dovetail
Lü Hui-ting;HAO Yan-hua;HUANG Zhi-jian;WU Fu-xian
..............page:1295-1300
Numerical evaluation of tandem rotor for highly loaded transonic fan
ZHAO Bin;LIU Bao-jie
..............page:1352-1361
Effects of flow orientations on the coking characteristic of jet fuel RP-3
WU Han;DENG Hong-wu;XU Guo-qiang;JU Yin-chao;SUN Ji-ning
..............page:1341-1345
Effects of temperature distribution and level on heat transfer on a rotating free disk
ZHAO Xi;XU Guo-qiang;LUO Xiang
..............page:1310-1320
Speed control design and test for piston EFI engine of unmanned helicopter
ZENG Guo-gui;LIAO Zhi-lin;KAN Zhao-cheng
..............page:1384-1388
Numerical simulation and hot test investigation of plug nozzle in solid rocket motor
REN Jun-xue;LIU Yu;LIAO Yun-fei;XIE Kan
..............page:1420-1425
Design and experiment for a GH2/GO2 fuel-rich preburner
LI Mao;GAO Yu-shan;CHEN Ze;JIN Ping;CAI Guo-biao
..............page:1426-1430
Experimental and computational investigation of single-expansion-ramp-nozzle
TAN Jie1;JIN Jie1;DU Gang1;XU Jing-lei2
..............page:1223-1230
Study on the correlative property of excitation on compressor rotor blades
FANG Li-cheng;LI Shun-ming;DU Jian-jian;CHEN Mo-li
..............page:1289-1294
UIO-based sensor fault diagnosis for aero-engine control systems
TAN Dao-liang;HE Ai;KONG Xiang-xing;WANG Xi
..............page:1396-1404
Experimental study on lean-blow-out of double/fuel-lean trapped vortex combustor
ZHANG Tao1;SONG Shuang-wen2;FAN Wei-jun1;ZHANG Rong-chun1
..............page:1328-1333
Numerical simulation of the dynamic process of aero-engine blade-to-case rub-impact
LIU Shu-guo;HONG Jie;CHEN Meng
..............page:1282-1288
Fatigue evaluation of helicopter transmission system
KANG Li-xia1;2;CAO Yi-hua1;NING Xiang-rong3
..............page:1431-1435
Acoustic properties of a slit resonator attached to a pipe with flow
DAI Xi-wen;JING Xiao-dong;SUN Xiao-feng
..............page:1231-1236