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Research progress in high thrust liquid oxygen methane rocket engine technology
Yonghua TAN
doi: 10.7527/S1000-6893.2024.29690
2024, (11): 529690-529690.
PDF [ 2166 K ]( 397 ) HTML
Research progress on key issues of adjustable inlet system for aerospace vehicles
Ziyun WANG, Hang YU, Yue ZHANG, Huijun TAN, Yi JIN, Xin LI
doi: 10.7527/S1000-6893.2023.29440
2024, (11): 529440-529440.
PDF [ 15634 K ]( 197 ) HTML
Research progress on structural strength of liquid rocket engine during engineering development phase
Penggang MU, Binchao LI, Jun WANG, Shaowei SONG, Hanyang SHI
doi: 10.7527/S1000-6893.2023.29065
2024, (11): 529065-529065.
PDF [ 3489 K ]( 178 ) HTML
Thermal structure technology development of rocket based combined cycle engine
Fei QIN, Zheng ZHAO, Guoqiang HE, Tingting JING, Xing SUN, Xianggeng WEI
doi: 10.7527/S1000-6893.2024.29572
2024, (11): 529572-529572.
PDF [ 8576 K ]( 135 ) HTML
Dual-mode scramjet: From performance optimization to mode-design
Jun CHEN, Hanchen BAI, Bing WAN, Qi LI
doi: 10.7527/S1000-6893.2024.29781
2024, (11): 529781-529781.
PDF [ 8439 K ]( 157 ) HTML
High frequency combustion instability in liquid rocket engines: Review
Guangxu WANG, Bin LI, Yonghua TAN, Yushan GAO
doi: 10.7527/S1000-6893.2023.29450
2024, (11): 529450-529450.
PDF [ 5723 K ]( 302 ) HTML
Analysis of structure and regime of ethylene fuel injection flame in circular⁃section supersonic combustor
Tao TANG, Jiangfei YU, Yuhui HUANG, Hongbo WANG, Mingbo SUN, Guoyan ZHAO, Dapeng XIONG, Zhenguo WANG
doi: 10.7527/S1000-6893.2023.28880
2024, (11): 528880-528880.
PDF [ 3966 K ]( 79 ) HTML
Improvement of thruster test plume pressure measurement system based on TRIZ theory
Chun CAO, Long YANG
doi: 10.7527/S1000-6893.2023.28613
2024, (11): 528613-528613.
PDF [ 4069 K ]( 44 ) HTML
Precise engine displacement testing technique based on stereo vision and circular mark points
Yushan GAO, Song YAN, Zhiwei ZHANG
doi: 10.7527/S1000-6893.2023.28826
2024, (11): 528826-528826.
PDF [ 4583 K ]( 929 ) HTML
Lightweight design of stiffening ribs layout of a bypass engine casing
Liang MENG, Jing ZHANG, Yadong WANG, Yang YU, Fan ZHANG, Jihong ZHU, Weihong ZHANG
doi: 10.7527/S1000-6893.2023.29021
2024, (11): 529021-529021.
PDF [ 5665 K ]( 129 ) HTML
Thermal protection and drag reduction characteristics of discrete hole film cooling in high Mach number combustor
Dingyuan WEI, Silong ZHANG, Jianfei WEI, Jingying ZUO, Xin LI, Wen BAO
doi: 10.7527/S1000-6893.2023.29075
2024, (11): 529075-529075.
PDF [ 7749 K ]( 63 ) HTML
3D grain reverse design and shape optimization for solid rocket motor
Wentao LI, Yunqin HE, Wenbo LI, Yiyi ZHANG, Guozhu LIANG
doi: 10.7527/S1000-6893.2023.29089
2024, (11): 529089-529089.
PDF [ 5414 K ]( 96 ) HTML
Experimental study on cavitating flow characteristics of inducer with inflow entrained non⁃condensable gas
Ronghao LIN, Hui CHEN, Le XIANG, Nianchong QU
doi: 10.7527/S1000-6893.2023.29095
2024, (11): 529095-529095.
PDF [ 4301 K ]( 45 ) HTML
Ignition characteristics and exhaust experiment of 120 N engine at simulated high lunar temperature
Ruida CHEN, Xiachao CHEN, Hongyu CHEN, Hui XU, Xin HONG
doi: 10.7527/S1000-6893.2023.29112
2024, (11): 529112-529112.
PDF [ 4657 K ]( 108 ) HTML
Effects of back pressure on atomization characteristics of impinging jet injector
Huibo WU, Anlong YANG, Feng ZHANG, Baoe YANG, Junkai LIAN, Chenglong TANG
doi: 10.7527/S1000-6893.2023.29213
2024, (11): 529213-529213.
PDF [ 3707 K ]( 60 ) HTML
Control volume free element method and its application in turbulent combustion
Jinxing DING, Huayu LIU, Xiaowei GAO
doi: 10.7527/S1000-6893.2024.29382
2024, (11): 529382-529382.
PDF [ 2499 K ]( 27 ) HTML
Effects of thermal nonequilibrium on hydrocarbon⁃fueled scramjets
You WU, Bing CHEN, Qingchun YANG, Xu XU
doi: 10.7527/S1000-6893.2023.29399
2024, (11): 529399-529399.
PDF [ 4681 K ]( 62 ) HTML
Self⁃excited oscillation and stability of flow regulator pipeline system
Meng DONG, Lixiang XING, Haohai XU
doi: 10.7527/S1000-6893.2023.29427
2024, (11): 529427-529427.
PDF [ 6465 K ]( 38 ) HTML
High pressure combustion experiment for hypergolic propellant unlike doublet injectors
Feng ZHANG, Yi SUN, Shuai SHANG, Baoe YANG
doi: 10.7527/S1000-6893.2023.29507
2024, (11): 529507-529507.
PDF [ 1991 K ]( 63 ) HTML
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