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Journal of Aerospace Power
1000-8055
2010 Issue 11
Thermo-viscoelastic stress analysis of rocket motor grain under durative cooling condition
WANG Yu-feng;LI Gao-chun;LIU Zhu-qing;DING Biao
..............page:2606-2611
Experiment of discharge coefficients for small scale cylindrical holes
ZHANG Xiao-wei;ZHU Hui-ren;ZHANG Xia;LI Zhong-zhou
..............page:2479-2485
Research on vibration characteristic of annular combustor in aero-engine
LUO Gui-huo;WU Hong-liang;NING Xiang-rong;ZHOU Hai-lun
..............page:2625-2631
Study on low cycle fatigue characteristic of single crystal notched specimens
ZHAO Ping;HE Qing-hua;LI Wei;LU Bo;Ding Zhi-ping
..............page:2632-2636
Control method of compressor stator vane angle for an aero-engine
SUI Yan-feng;BING Lian-xi;SHI Lei;RONG Li
..............page:2589-2593
Study on high-loading turbine airfoil design based on flow control
CHEN Ping-ping;QIAO Wei-yang;HOU Wei-tao;LUO Hua-ling
..............page:2528-2538
Numerical investigation of the laminar and drag-reduction control by using suction technology on a supercritical airfoil
HE Yu-wei;LIU Pei-qing;DUAN Hui-shen;WANG Wen-hu
..............page:2443-2449
Investigation on the heat flux of heat sink chamber
GAO Yu-shan;DU Zheng-gang;JIN Ping;CAI Guo-biao
..............page:2619-2624
Numerical simulation of convective heat transfer inside film cooling hole
XIE Jie;ZHANG Jing-zhou;TAN Xiao-ming;SHI Rui
..............page:2507-2513
Modeling and simulation research of turboprop engine control technology
TIAN Chao;HUANG Xiang-hua;DENG Zhi-wei
..............page:2599-2605
Quantity method of technical risk assessment for civil aero-engine
TU Qiu-ye;ZHANG Wei;CAI Yuan-hu;ZHOU Li
..............page:2403-2408
Boundary transition research of scramjet inlet based on the Tollmien-Schlichting (T-S) wave syntony
ZHAO Jun-bo;SHEN Qing;ZHANG Hong-jun;BAI Kui
..............page:2420-2424
Effect of inlet distortion on the stability of a transonic compressor with casing treatment
CHEN Mei-ning;PIAO Ying;WANG Da-lei
..............page:2578-2583
Influence of afterburning on infrared signature of rocket motor exhaust plume
WANG Wei-chen;WEI Zhi-jun;ZHANG Qiao;WANG Ning-fei
..............page:2612-2618
Test model of intake air amount on rotary engine of unmanned aerial vehicle
TANG Ting-xiao;ZHAO Hou-liang;CHEN Huai-hai
..............page:2425-2430
Conceptual research on waverider design for aerospace vehicle
LIU Yan-bin;YAO Ke-ming;LU Yu-ping
..............page:2409-2414
Blockage area rule for multi-stage axial compressor meridional channel
CUI Jian;CHENG Zhao-qing;YANG Chun;LIU Ying-long;ZHOU Sheng
..............page:2520-2527
Aerodynamic design and numerical validation of highly loaded fan
XU Peng-fei;ZHAO Bin;LIU Bao-jie
..............page:2548-2555
Aerodynamic design of highly loaded fan Analysis of rotor tip parameter selection
ZHAO Bin;XU Peng-fei;LIU Bao-jie
..............page:2564-2570
Quantitative analysis and numerical simulation of optimization of a propulsion system
ZHANG Wei;CAI Yuan-hu;SU San-mai;TU Qiu-ye
..............page:2450-2456
Numerical simulation of lateral jet interaction flow field in supersonic/hypersonic flow
YANG Xi-xiang;FEI Yang;JIANG Zhen-yu;ZHANG Wei-hua
..............page:2437-2442
Analysis of inerting process influenced by scrubbing efficiency in aircraft fuel tank
FENG Shi-yu;LU Shi-hua;LIU Wei-hua;JIANG Jun-chang;LIU Su-yan
..............page:2457-2463
Numerical studies of temperature drop and pressure loss in a cover-plate preswirl system
ZHU Xiao-hua;LIU Gao-wen;LIU Song-ling;FENG Qing
..............page:2498-2506
Numerical simulation on inlet distortion of centrifugal compressor with 90° bent pipe
LI Du;YANG Ce;CHEN Shan;QI Ming-xu
..............page:2556-2563
Conception research of CO2 gasdynamic laser based on turbojet
WANG Jian;CHEN Jian-ping;LIU Xiao-jun;GU Ting-ting
..............page:2415-2419
Dynamic response of torsional vibration of gear-rotor with random parameters
WEI Yong-xiang;CHEN Jian-jun;WANG Min-juan
..............page:2637-2642
Aero-engine fault diagnosis based on Boosting-SVM
SUN Chao-ying;LIU Lu;LIU Chuan-wu;WEI Xun-kai
..............page:2584-2588