Journal of Aerospace Power 2010 Issue 7 Aero-engine high stability control scheme design based on angle of attack predictive model

Aero-engine high stability control scheme design based on angle of attack predictive model
CHEN Ting-hao;ZHANG Hai-bo;SUN Jian-guo

..............page:1676-1682

Coupled heat transfer calculation on an airfoil electrothermal anti-icing surface
BU Xue-qin;LIN Gui-ping;YU Jia

..............page:1491-1496

Algorithm for determination of the initial point in error tooth contact analysis
TANG Jin-yuan;LEI Guo-wei

..............page:1670-1675

Numerical simulation on a film-cooled rotating model with 30° injection holes
YANG Bin;XU Guo-qiang;TAO Zhi;DING Shui-ting;WU Hong-wei

..............page:1443-1453

Effect of spillage slot on the performance of two-dimensional hypersonic inlet
ZHAO Liang;YUAN Hua-cheng;LI Bo

..............page:1573-1580

Investigation on root blade profile of a large meridional expansion turbine
TANG Hong-fei;HUANG Hong-yan;WANG Zhen-feng;HAN Wan-jin

..............page:1602-1608

Numerical research on flow dynamics and infrared radiation characteristics for scaled chevron convergent nozzle
PAN Cheng-xiong;ZHANG Jing-zhou;SHAO Wan-ren;SHAN Yong

..............page:1518-1523

Research on wing structure deformation for aerodynamic force and inertial force of flapping-wing
ZHANG Ya-feng;SONG Wen-ping;SONG Bi-feng;ZHANG Wei

..............page:1561-1566

Experimental research on film cooling characteristics of cylindrical hole and expanding hole on the leading edge
ZHU Hui-ren;ZHANG Xia;LIU Cun-liang

..............page:1464-1470

Mesh stiffness function and stability analysis for parametric vibration of spiral bevel gears
WANG Yan-zhong;ZHOU Yuan-zi;LI Guo-quan;GUO Mei

..............page:1664-1669

Theoretical analysis of steady-state operating characteristics of a cryogenic loop heat pipe
BAI Li-zhan;LIN Gui-ping

..............page:1530-1535

Reduction of detailed reaction mechanism using methods based on simulations of perfectly stirred reactor
WANG Hui-ru;JIN Jie

..............page:1497-1505

Investigation of cold flow field of a multi-injection combustor with different geometries
WU Yao-zeng;HUANG Yong;WANG Fang;ZHANG Yu-fang

..............page:1536-1544

Unsteady numerical investigation of the influence of axial gap on the turbine loss
ZHOU Li;ZHANG Xin;CAI Yuan-hu

..............page:1595-1601

Study of wall temperature on the interstage turbine single vortex combustor
ZHANG Rong-chun;FAN Wei-jun;XING Fei

..............page:1512-1517

Numerical research of ice accretion on two-dimensional airfoils
SUN Zhi-guo;ZHU Cheng-xiang;FU Bin;ZHU Chun-ling

..............page:1485-1490

Investigation of a variable geometry scramjet inlet with a rotating cowl operating in a large Mach number range
JIN Zhi-guang;ZHANG Kun-yuan

..............page:1553-1560

Investigation of rolling bearing fault diagnosis based on scale-based concurrent matrix
QIN Hai-qin;XU Ke-jun;SUI Yu-song;JIA Ming-ming

..............page:1628-1633

Small scale mixing enhancement of fuel/air using multi-source vortex technology
ZHANG Yu-fang;HUANG Yong;WANG Fang;WU Yao-zeng;XIAO Ying

..............page:1506-1511

Robust performance analysis of mistuned bladed disks
YAO Jian-yao;WANG Jian-jun;LI Qi-han

..............page:1634-1639

Analysis on acoustic longitudinal oscillation frequency in combustion chamber with sudden change sections
ZHANG Qiao;LI Jun-wei;WANG Ning-fei

..............page:1653-1658

Numerical prediction of lean blowout in aero-engine combustor
CAI Wen-xiang;ZHAO Jian-xing;HU Hao-sheng;DANG Xin-xian;WU Xiao-song

..............page:1478-1484

Design and experimental study on whirl aero-valve for pulse detonation engine
ZHENG Dian-feng;YANG Yi-yong;WANG Jia-hua

..............page:1471-1477

Measured overall effusion cooling effectiveness over a wide blowing ratio range using infrared imaging
ZHANG Chi;SONG Bo;LIN Yu-zhen;XU Quan-hong;LIU Yan

..............page:1454-1463

Cavity flow oscillations and aeroacoustic characteristics at supersonic speeds
YANG Dang-guo;FAN Zhao-lin;LI Jian-qiang;JIANG Wei-min;TIAN Jun

..............page:1567-1572

Effect of the holes array arrangement on the full coverage film cooling characteristics
YANG Cheng-feng;ZHANG Jing-zhou;YANG Wei-hua

..............page:1524-1529

Effects of degree of sidewall shade on performance of two-dimentional supersonic inlet with non-sideslip
ZHANG Long-dong;ZHANG Kun-yuan;NAN Xiang-jun

..............page:1581-1587

Study on virtual test technology of liquid propellant engine
DUAN Na;ZHANG Li-hui;XU Shan-shan;ZHU Zi-huan;YU Hai-lei

..............page:1659-1663

Research on environmental factor based on degradation data
FENG Jing;ZHOU Jing-lun

..............page:1622-1627

Numerical investigation about the effect of a partial circumference casing treatment on a compressor
LIU Jian-yong;YUAN Wei;LU Ya-jun

..............page:1609-1614

Test system design for small H2/O2 rocket engine
LIU Wan-long;DIAO Peng;WANG Chong;LIANG Guo-zhu;ZHANG Xue-jun

..............page:1646-1652

hang kong dong li xue bao zheng gao jian ze

..............page:封3

Numerical simulation on flow and heat transfer of elliptical pin-fins in cooling channel
DENG Ding-yuan;GAO Hang-shan;YU Kua-hai;YUE Zhu-feng

..............page:1545-1552

Quantitative research on performance degradation of single-stage compressor
LI Ben-wei;LI Dong;LI Jiang-hua;WANG Yong-hua;YANG Xin-yi

..............page:1588-1594

Optimal calibration interval of test system based on reliability index
HAN Xu;ZU Xian-feng;CAI Ying-bo

..............page:1640-1645

Influence of shock/tip leakage vortex interaction on flow stability in a single-stage transonic axial compressor
ZHANG Zhuo-xun;WU Yan-hui;CHU Wu-li;ZHANG Hao-guang

..............page:1615-1621