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科研机构
北京航空航天大学 [39]
重庆大学 [1]
内容类型
期刊论文 [22]
会议论文 [18]
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2019 [1]
2018 [3]
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2016 [6]
2015 [8]
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Numerical and experimental investigations on injection effects of orifice injector plate in hybrid rocket motors
期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 162, 页码: 275-283
作者:
Zhu, Hao
;
Li, Meng
;
Tian, Hui
;
Wang, Pengfei
;
Yu, Nanjia
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Hybrid rocket motor
Orifice injector plate
Experimental investigation
Numerical simulation
Unsteady simulation and experimental study of hydrogen peroxide throttleable catalyst hybrid rocket motor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 76, 页码: 27-36
作者:
Zhao, Bo
;
Yu, Nanjia
;
Liu, Yufei
;
Zeng, Peng
;
Wang, Jue
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/12/30
Hybrid rocket motor
Thrust regulation process
Motor performance
Unsteady simulation
Test firings
Numerical and experimental investigations of single-element and double-element injectors using gaseous oxygen/gaseous methane
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 75, 页码: 24-34
作者:
Yu, Nanjia
;
Zhang, Yang
;
Li, Feng
;
Dai, Jian
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
F/O momentum ratio
Injector
Gaseous oxygen/gaseous methane
Planar laser induced fluorescence (PLIF)
Combustion
Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 77, 页码: 725-732
作者:
Dai Jian
;
Cai GuoBiao
;
Zhang Yang
;
Yu NanJia
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Liquid rocket engine
Shear coaxial injector
Computational fluid dynamics
Non-intrusive optical diagnostics
Parametric study and performance analysis of hybrid rocket motors with double-tube configuration
期刊论文
ACTA ASTRONAUTICA, 2017, 卷号: 132, 页码: 90-96
作者:
Yu, Nanjia
;
Zhao, Bo
;
Lorente, Arnau Pons
;
Wang, Jue
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Vortex cooling
Thrust chamber performance
Numerical simulation
Test firings
Geometric effects of fuel regression rate in hybrid rocket motors
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 页码: 807-813
作者:
Cai GuoBiao
;
Zhang YuanJun
;
Wang PengFei
;
Hui Tian
;
Zhao Sheng
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
geometric effect
regression rate
hydraulic diameter
hybrid rocket motor
Experimental investigations of coaxial injectors in a laboratory-scale rocket combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 59, 页码: 41-51
作者:
Dai Jian
;
Cai GuoBiao
;
Zhang Yang
;
Yu NanJia
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2019/12/30
Liquid rocket engine
Shear coaxial injector
Turbulent combustion
Non-intrusive optical diagnostics
Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor
期刊论文
ACTA ASTRONAUTICA, 2016, 卷号: 119, 页码: 137-146
作者:
Sun, Xingliang
;
Tian, Hui
;
Li, Yuelong
;
Yu, Nanjia
;
Cai, Guobiao
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  |  
浏览/下载:1/0
  |  
提交时间:2019/12/30
Regression rate behavior
Propellant combinations
Hybrid rocket motor
Test and simulation
Effect of grain port length-diameter ratio on combustion performance in hybrid rocket motors
期刊论文
ACTA ASTRONAUTICA, 2016, 卷号: 128, 页码: 83-90
作者:
Cai, Guobiao
;
Zhang, Yuanjun
;
Tian, Hui
;
Wang, Pengfei
;
Yu, Nanjia
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
Length-diameter ratio
Hybrid rocket motor
Combustion performance
Regression rate
Experimental and simulation study of a Gaseous oxygen/Gaseous hydrogen vortex cooling thrust chamber
期刊论文
ACTA ASTRONAUTICA, 2016, 卷号: 118, 页码: 11-20
作者:
Yu, Nanjia
;
Zhao, Bo
;
Li, Gongnan
;
Wang, Jue
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Vortex cooling
Thrust chamber performance
Numerical simulation
Test firings
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