航空动力学报

火箭发动机

Investigation of base load characteristics during aerodynamic reentry phase of super heavy starship

LIN Xiaohui, GAO Wuhuan, QIN Tong, CHEN Liwei, CHU Yihui, XUE Fei, GU Yuanfu, XU Changyue

2026, 41(5): 20250221. doi: 10.13224/j.cnki.jasp.20250221

[Abstract] [FullText HTML] [PDF 37359KB] [Cited By]
Study on dynamic characteristics of gas-liquid internal mixing injector under backpressure

LYU Xiuwen, ZHAO Nannan, QIAO Wentong, ZHANG Bingbing, SHI Jingyan, FU Qingfei

2026, 41(5): 20250228. doi: 10.13224/j.cnki.jasp.20250228

[Abstract] [FullText HTML] [PDF 4138KB] [Cited By]
Numerical simulation of acoustic mode characteristics of combustion chamber considering influence of dome

ZHANG Zehao, DONG Libao, ZHAO Liyou, GUO Kangkang, PANG Jianguo

2026, 41(4): 20250119. doi: 10.13224/j.cnki.jasp.20250119

[Abstract] [FullText HTML] [PDF 2086KB] [Cited By]
Performance comparison between subsonic and supersonic needle gas valves

HUANG Chujiu, WEI Zhijun, LI Zhiyuan, GAO Ziqing, LI Dalin

2026, 41(1): 20240855. doi: 10.13224/j.cnki.jasp.20240855

[Abstract] [FullText HTML] [PDF 3567KB] [Cited By]
Ground direct-connection experiment of low-thrust magnesium powder water ramjet

CHEN Hong, FANG Xiaobo, LIU Conglin, LIU Changmeng, LI Xianhui, SHAN Yongzhi

2026, 41(1): 20250004. doi: 10.13224/j.cnki.jasp.20250004

[Abstract] [FullText HTML] [PDF 4813KB] [Cited By]
Influence of cold launch bullet body deflection on the force and thermal environment of launch vehicles

SUN Zhongyi, CUI Yangwen, ZHAO Chengeng, LE Guigao

2025, 40(11): 20230767. doi: 10.13224/j.cnki.jasp.20230767

[Abstract] [FullText HTML] [PDF 20063KB] [Cited By]
Development and on-orbit verification of bipropellant accurate attitude control 10 N rocket engine

CAI Kun, WANG Fengshan, YANG Shangfeng, WANG Ping, GUAN Changbin, ZHANG Zhen, YAO Zhaopu, MAO Xiaofang

2025, 40(11): 20240067. doi: 10.13224/j.cnki.jasp.20240067

[Abstract] [FullText HTML] [PDF 7231KB] [Cited By]
Mechanism of “heat-acoustic-vortex” coupling for transverse unstable combustion in an O₂/CH₄ rectangle rocket combustor

CAO Wei, GUO Kangkang, REN Yubin, TONG Yiheng, LIN Wei, HUANG Weidong, NIE Wansheng

2025, 40(11): 20240608. doi: 10.13224/j.cnki.jasp.20240608

[Abstract] [FullText HTML] [PDF 17982KB] [Cited By]
Ignition impact characteristics of LOX/LCH₄ coaxial injectors

LIU Yunhao, WANG Chunmin, FENG Yuanxiang, LIU Zhaoyu, LI Longfei

2025, 40(11): 20250036. doi: 10.13224/j.cnki.jasp.20250036

[Abstract] [FullText HTML] [PDF 2082KB] [Cited By]
Numerical investigation on design and aerodynamic parameters of rocket sled sabot backing ring

HAO Fenfen, ZHOU Xuewen, CHENG Mingcan, YANG Yang, PANG Chao

2025, 40(11): 20250040. doi: 10.13224/j.cnki.jasp.20250040

[Abstract] [FullText HTML] [PDF 3254KB] [Cited By]
Simulation research of Pogo suppression of liquid rocket based on fluid active control method

WU Chujun, JIAO Zongxia, XU Yuanzhi, WU Shaodong, PAN Hui, HU Jiuhui

2025, 40(10): 20240047. doi: 10.13224/j.cnki.jasp.20240047

[Abstract] [FullText HTML] [PDF 3558KB] [Cited By]
Combustion process of agglomerated boron particles at 0.1—1.0 MPa atmospheric pressure

CHEN Binbin, DUAN Lian, YANG Gan, MA Likun, FENG Yunchao, XIA Zhixun

2025, 40(9): 20240817. doi: 10.13224/j.cnki.jasp.20240817

[Abstract] [FullText HTML] [PDF 5395KB] [Cited By]
Numerical study on drag coefficient of deformable alumina droplet in compressible flows

DING Shuai, HU Haiyang, WANG Qiang

2025, 40(7): 20230307. doi: 10.13224/j.cnki.jasp.20230307

[Abstract] [FullText HTML] [PDF 3686KB] [Cited By]
Propulsion system design method for multi-object kill vehicles based on guidance strategy

LI Wentao, LI Wenbo, HE Yunqin, ZHANG Yiyi, ZHENG Hanyun, LIANG Guozhu

2025, 40(7): 20240219. doi: 10.13224/j.cnki.jasp.20240219

[Abstract] [FullText HTML] [PDF 11504KB] [Cited By]
Simulation study on the spray and mixing characteristics of a liquid-liquid throttleable pintle injector

LUAN Shaolei, WU Jiping, ZHANG Jiaqi, CHENG Peng, XIE Yu

2025, 40(7): 20240230. doi: 10.13224/j.cnki.jasp.20240230

[Abstract] [FullText HTML] [PDF 26860KB] [Cited By]
Simulation study on the influence of ignition cartridge location on ignition process in solid rocket motor

TAN Zhijie, LI Junwei, QIN Shengfu, WANG Ningfei

2025, 40(6): 20230705. doi: 10.13224/j.cnki.jasp.20230705

[Abstract] [FullText HTML] [PDF 2794KB] [Cited By]
Fluid simulation of plasma characteristics in radio frequency ion thrusters

CUI Yunwei, REN Junxue, ZHANG Guangchuan, CAO Lehui, LIU Xuanlin, TANG Haibin

2025, 40(6): 20240090. doi: 10.13224/j.cnki.jasp.20240090

[Abstract] [FullText HTML] [PDF 2492KB] [Cited By]
Plume flow field and base heating environment of the multi-nozzle rocket in ascent phase

REN Fantao, JIANG Yi, LIU Hanyu, JIA Qiming

2025, 40(5): 20230575. doi: 10.13224/j.cnki.jasp.20230575

[Abstract] [FullText HTML] [PDF 5025KB] [Cited By]
Fuel supply characteristics of powder fuel engine

DU Xinlei, DONG Xingang, HUANG Likeng, HE Jingxuan, TIAN Linghan, WANG Zongtao

2025, 40(5): 20230578. doi: 10.13224/j.cnki.jasp.20230578

[Abstract] [FullText HTML] [PDF 946KB] [Cited By]
Experiment on longitudinal combustion instability of a hypergolic propellant model engine

CHU Wei, JIANG Chuanjin, REN Yongjie, TONG Yiheng, XU Boqi, GUO Kangkang, NIE Wansheng

2025, 40(5): 20230580. doi: 10.13224/j.cnki.jasp.20230580

[Abstract] [FullText HTML] [PDF 24942KB] [Cited By]
Numerical study on pure rocket mode performance characteristics of a RBCC engine

LING Wenhui, WEI Baoxi, HOU Jinli, YAO Dahao, LUO Feiteng

2025, 40(5): 20240433. doi: 10.13224/j.cnki.jasp.20240433

[Abstract] [FullText HTML] [PDF 34789KB] [Cited By]
Comparison of flow characteristics between tank-to-tank and tank-to-manifold crossfeed systems for liquid rocket

DU Feiping, LI Cui, CHENG Yiwei, WU Dinghang, LI Yanzhong, XU Yuanyuan

2025, 40(4): 20220666. doi: 10.13224/j.cnki.jasp.20220666

[Abstract] [FullText HTML] [PDF 3024KB] [Cited By]
Simulation study on thrust effect of ionic wind

CHEN Yuhang, LI Ting

2025, 40(3): 20220661. doi: 10.13224/j.cnki.jasp.20220661

[Abstract] [FullText HTML] [PDF 3871KB] [Cited By]
Experimental study on two-stage propulsion monorail rocket sled

XIA Youcai, KONG Weihong, SUN Qihui, ZhANG Hao, LIU Kuixian, AN Mingming, LI Junyao, MA Jun

2025, 40(3): 20230370. doi: 10.13224/j.cnki.jasp.20230370

[Abstract] [FullText HTML] [PDF 1325KB] [Cited By]
Research trends of pre-cooled turbo engine and a wide-range scheme of pre-cooled turbo combined cycle power

YAO Zhaohui, GUO Yuanzhao, HE Weifeng, YU Tianhao, CHEN Jia, BAO Wen

2025, 40(2): 20220446. doi: 10.13224/j.cnki.jasp.20220446

[Abstract] [FullText HTML] [PDF 1207KB] [Cited By]
Effects of acceleration overload on combustion characteristics of HTPB/AP/Al propellant

HE Ye, LI Junwei, TIAN Zhongliang, QIN Shengfu, XU Tuanwei, DING Miao, WANG Ningfei

2024, 39(8): 20220067. doi: 10.13224/j.cnki.jasp.20220067

[Abstract] [FullText HTML] [PDF 10494KB] [Cited By]
Effect of blockage rate on spray characteristics of liquid-liquid pintle multi-injector elements

WANG Kai, TANG Liang, LEI Fanpei, YANG Anlong, ZHOU Lixin

2024, 39(7): 20220419. doi: 10.13224/j.cnki.jasp.20220419

[Abstract] [FullText HTML] [PDF 8909KB] [Cited By]
Numerical simulation of liquid film converge characteristics of bipropellant pressure swirl injector

WU Jiaman, LIU Yong, ZHANG Xiang

2024, 39(3): 20210478. doi: 10.13224/j.cnki.jasp.20210478

[Abstract] [FullText HTML] [PDF 1941KB] [Cited By]
Research progress on system oscillation and stability of liquid rocket engine

DONG Meng, TAN Yonghua, XING Lixiang, XU Haohai

2023, 38(12): 2919-2936. doi: 10.13224/j.cnki.jasp.20220036

[Abstract] [FullText HTML] [PDF 2334KB] [Cited By]
Simulation of liquid oxygen temperature and its influence on acoustic frequency of swirl injector

ZHANG Ya, TIAN Yuan, PAN Liang

2023, 38(11): 2785-2790. doi: 10.13224/j.cnki.jasp.20220022

[Abstract] [FullText HTML] [PDF 1526KB] [Cited By]
Test and simulation of film cooling length in conventional propellant rocket engine

HOU Ruifeng, CHEN Jianhua, LI Longfei, YANG Jianwen, ZHANG Guodong

2023, 38(11): 2799-2808. doi: 10.13224/j.cnki.jasp.20230038

[Abstract] [FullText HTML] [PDF 6440KB] [Cited By]
Influence of dynamic lateral overload on internal ballistics of solid rocket motor

TIAN Zhongliang, LI Junwei, HE Ye, WANG Ningfei

2023, 38(2): 504-512. doi: 10.13224/j.cnki.jasp.20210442

[Abstract] [FullText HTML] [PDF 4854KB] [Cited By]
Analysis of JT refrigeration influence on temperature control of mainstream liquid in cryogenic storage tank

ZHOU Zhenjun, LIU Xin, LIU Chen, MENG Nan, CHEN Shikui

2022, 37(9): 2001-2008. doi: 10.13224/j.cnki.jasp.20210212

[Abstract] [FullText HTML] [PDF 1597KB] [Cited By]
Anomaly detection method of liquid rocket engine based on incremental isolation forest

ZHANG Wanxuan, XUE Wei, ZHANG Nan

2022, 37(8): 1674-1682. doi: 10.13224/j.cnki.jasp.20220119

[Abstract] [FullText HTML] [PDF 3153KB] [Cited By]
Preliminary analysis on the demand of nuclear fusion space thruster

SONG Jun

2022, 37(7): 1495-1502. doi: 10.13224/j.cnki.jasp.20210122

[Abstract] [FullText HTML] [PDF 754KB] [Cited By]
Gas-solid two-phase flow characteristics of SRM propellant with front and rear wings

ZHANG Jun, QIN Lei, GAO Tianyu, WANG Minghua, JIN Shenxin, GAO Puqing

2022, 37(3): 664-672. doi: 10.13224/j.cnki.jasp.20210137

[Abstract] [FullText HTML] [PDF 1579KB] [Cited By]
Design of dual-bell nozzles with different extension pressure distributions

LIU Yazhou, LI Ping, CHEN Hongyu, YANG Jianwen, CHEN Yidan

2022, 37(2): 424-432. doi: 10.13224/j.cnki.jasp.20210096

[Abstract] [FullText HTML] [PDF 3743KB] [Cited By]
Impact of ignition charge on ignition process of dual-pulse solid rocket motor

XIA Dingguo, XU Guiyang, WEI Zhijun, ZHANG Weiqi

2022, 37(2): 433-442. doi: 10.13224/j.cnki.jasp.20210131

[Abstract] [FullText HTML] [PDF 4028KB] [Cited By]
Reconfiguration control of launch vehicle based on Armijo criterion and BFGS algorithm

YU Haisen, TAN Shujun, WU Zhigang

2022, 37(1): 204-213. doi: 10.13224/j.cnki.jasp.20210059

[Abstract] [FullText HTML] [PDF 1543KB] [Cited By]
Optimization design for nozzle contour of rocket engine based on response surface method

WANG Yingpeng, XU Yihua, SUN Haijun, FENG Xiping

2022, 37(1): 214-224. doi: 10.13224/j.cnki.jasp.20210004

[Abstract] [FullText HTML] [PDF 1630KB] [Cited By]
Numerical simulation on three-dimension supersonic jet of missile vertical launching system

XU Yue, ZHANG Zhen-peng, TIAN Ai-mei, CHEN Xiao-qing

2007, 22(10): 1765-1770.

[Abstract] [FullText HTML] [PDF 1873KB] [Cited By]
Aerodynamic analysis and wind tunnel testing on maglev launch assist

CHEN Xiao-dong, YANG Wen-jiang, LIU Yu, DUAN Yi

2007, 22(9): 1560-1564.

[Abstract] [FullText HTML] [PDF 576KB] [Cited By]
Research on influence of diameter ratio and length-diameter ratio on structural integrity of solid propellant under temperature loading

YU Yang, WANG Ning-fei, ZHANG Ping

2007, 22(9): 1565-1568.

[Abstract] [FullText HTML] [PDF 1032KB] [Cited By]
Optimization of response surface of secondary gas injection thrust vector control

WU Xiong, WANG Zhong-wei, JIAO Shao-qiu, ZHANG Wei-hua

2007, 22(9): 1569-1572.

[Abstract] [FullText HTML] [PDF 284KB] [Cited By]

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Sponsor: Aviation Industry Corporation of China

Sponsored by: Chinese Society of Aeronautics Beijing University of Aeronautics and Astronautics

ISSN: 1000-8055 CN: 11-2297/V

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