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Journal of Aerospace Power
1000-8055
2012 Issue 9
Stall improvement mechanism of vaneless diffuser flow path control in a centrifugal compressor
WANG Yong-sheng1;2;TONG Zhi-ting1;LIN Feng1;NIE Chao-qun1
..............page:2106-2112
System simulation and optimal design of hybrid rocket motor with pump feed system
ZHU Hao;KONG De-shuai;CAI Guo-biao
..............page:2128-2133
Thermo-structure integrative computation for nozzle in SRM
ZHENG Xiao-ya1;WANG Wei-xiang2;CAI Fei-chao1;CHEN Feng-ming1
..............page:2122-2127
Mathematical model of isentropic expansion process based on Φ function
ZHENG Hai-fei;TANG Hao
..............page:2035-2040
Flutter analysis of a two-dimensional wing with aerodynamic and structural nonlinearity
WANG Yi-feng1;SHAO Song2;ZHU Qing-hua2;ZHANG Cheng-lin2
..............page:2063-2074
Investigation of priming process of propellant lines using Fourier spectral method
CHEN Hong-yu;LIU Hong-jun CHEN Jian-hua;LIU Shang
..............page:2134-2139
Numerical simulation of an aero-engine fan with inlet distortion
LIU Yong-quan1;LIU Huo-xing2;ZHENG Ning1
..............page:2099-2105
Evaluation methods of the fuel mixing efficiency for Scramjet
ZHANG Wan-zhou1;2;LE Jia-ling2;TIAN Ye2;YANG Shun-hua2; DENG Wei-xin1;2;CHENG Wen-ming1
..............page:1958-1966
Experiment on multi-tube air-breathing two phase pulse detonation engine
ZHANG Qun;FAN Wei
..............page:1935-1938
Evaluation of multi-process plans based on fuzzy comprehensive evaluation and grey relational analysis
WANG Pei1;ZHANG Ding-hua1;CHEN Bing1;LI Shan1;MA Guan-ghui2 Company Limited; Aviation Industry Corporation of China;Xi’an 710021;China)
..............page:2075-2085
Calculation of start-up pressure of two-wheel bootstrap air cycle machine with foil air bearing
ZHAO Yun-feng;HU Wen-chao;ZHU Gang;NING Jia-qiang
..............page:2155-2160
Effects of equivalence ratio and gap size on the propagation behavior of detonations
ZHANG Chao;TANG Hao;LI Ming;Sudip Bhattrai
..............page:1948-1957
Design research of small flow rate multi-stage high-loaded axial compressor
XIE Ya-dong;SHAN Peng
..............page:2113-2121
Large-eddy simulation of two-phase reacting flows and combustion performance in model combustor
HE Yue-long1;DENG Yuan-hao2;YAN Ying-wen2; LI Jiang-hua2;ZHAO Jian-xing2
..............page:1939-1947
Effect of internal combustion wave rotor technology on performance of gas turbine engine
LI Jian-zhong1;2;GONG Er-lei1;WEN Quan2;WANG Jia-hua1
..............page:1928-1934
Research of water hammer and its suppression methods for spacecraft propulsion system
YAN Zheng;PENG Xiao-hui;CHENG Yu-qiang;WU Jian-jun
..............page:2028-2034
Modified reduced model for rapid analysis of tip clearance of high pressure turbine
YANG Xiao-guang;HUANG Jia
..............page:2048-2055
Research on aerodynamic characteristics of autorotating coaxial twin-rotor
JI Le-qiang;ZHU Qing-hua;Cui Zhao;LI Jian-bo
..............page:2013-2020
Disturbance rejection control method for turboshaft engines based on LQ/H_∞
LIAO Guang-huang1;2;LI Qiu-Hong1;LU Chen-hao1;HUANG Jin-quan1
..............page:2140-2146
Simulating and validating the stress-strain curve of the matrix cracking of ceramic matrix composite
SUN Zhi-gang;MIAO Yan;SONG Ying-dong
..............page:2056-2062
Experiment of in-cylinder mixture formation process low-pressure GDI engine
HU Chun-ming1;2;LI Ji-qi1;BAI Hong-lin2; REN Li-hong1;DONG Liang-liang1
..............page:1921-1927
Location method of acoustic emission source in non-uniform temperature field
CHEN Ya-nong1;HE Tian2;XIAO Deng-hong2;LIU Xian-dong2
..............page:2086-2092
Experiments of plasma assisted combustion’s effect on combustion products
ZHAO Bing-bing1;ZHANG Peng2;HE Li-ming1;DU Hong-liang1
..............page:1974-1978
Research on local DQ-Lagrange method for solving flow field in step flow
SUN Dan1;YANG Jian-gang2;ZHAO Huan1;LI Guang-chao1
..............page:1997-2003
Breakup characteristics and surface wave phenomenon of round liquid jets in crossflows
WANG Xiong-hui;HUANG Yong;WANG Fang; WANG Shao-lin;LIU Zhi-lin
..............page:1979-1987
Design of streamline-traced hypersonic inlets based on two-dimensional curved surface basic flowfield
LI Yong-zhou;ZHANG Kun-yuan;WANG Lei; NAN Xiang-jun;ZHANG Lin
..............page:2004-2012