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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
力学研究所 [8]
工程热物理研究所 [6]
长春光学精密机械与物... [1]
西安光学精密机械研究... [1]
兰州化学物理研究所 [1]
采集方式
OAI收割 [17]
内容类型
期刊论文 [15]
会议论文 [2]
发表日期
2024 [1]
2023 [4]
2022 [2]
2021 [1]
2020 [1]
2016 [2]
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学科主题
Engineerin... [1]
Materials ... [1]
材料科学与物理化学 [1]
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浏览/检索结果:
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Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units
期刊论文
OAI收割
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18
作者:
Pan JJ(潘俊杰)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wang RY(王若岩)
;
Wu K(吴坤)
  |  
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2024/05/27
modular unit
modification
regression rate
combustion efficiency
hybrid rocket engine
Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
期刊论文
OAI收割
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680
作者:
Qu DD(屈丹丹)
;
Lin X(林鑫)
;
Zhang K(张坤)
;
Li ZY(李志永)
;
Wang ZZ(王泽众)
  |  
收藏
  |  
浏览/下载:111/0
  |  
提交时间:2023/09/05
Hybrid rocket engine
additive manufacturing
three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
>
Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets
期刊论文
OAI收割
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19
作者:
Wang, Ruoyan
;
Lin, Xin
;
Wang, Zezhong
;
Wu, Kun
;
Zhang, Zelin
  |  
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2023/10/30
hybrid rocket engine
swirl-radial injection
regression rate
flame images
combustion efficiency
Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation
期刊论文
OAI收割
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113
作者:
He CM(何成明)
;
Zhang, Peng
;
He, Zhixia
;
Yue LJ(岳连捷)
  |  
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2023/04/20
Liquid rocket engine
Pintle injector
Spray characteristics
Jet film injection
Voronoi tessellation
Research on Rocket Engine Pose Measurement Technology Based on Monocular Vision
会议论文
OAI收割
Nanjing, China, 2023-06-16
作者:
Zhang, Haifeng
;
Wu, Jiaxin
;
Liu, Delian
;
Duan, Jiaxin
;
Guo, Gao
  |  
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2023/12/26
Rocket Engine
Centroid
Pose Measurement
Translation Vector
Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain
期刊论文
OAI收割
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
作者:
Zhang, Zelin
;
Lin, Xin
;
Wang, Zezhong
;
Wu, Kun
;
Luo, Jiaxiao
  |  
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2022/11/08
Hybrid rocket engine
Swirl injection
Novel composite fuel grain
Regression rate
Oxidizer-to-fuel ratio
Three-dimensional printed metal-nested composite fuel grains with superior mechanical and combustion properties
期刊论文
OAI收割
VIRTUAL AND PHYSICAL PROTOTYPING, 3, 2022, 卷号: 17, 页码: 437
作者:
Lin X(林鑫)
;
Qu DD(屈丹丹)
;
Chen XD(陈雪冬)
;
Wang ZZ(王泽众)
;
Luo JX(罗家枭)
  |  
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2022/10/23
Hybrid rocket engine
additive manufacturing
metal-nested composite fuel grain
mechanical properties
combustion properties
optical emission spectroscopy
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy
期刊论文
OAI收割
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
作者:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Peng JL(彭锦龙)
;
Liu, Yan
  |  
收藏
  |  
浏览/下载:48/0
  |  
提交时间:2021/11/01
Hybrid rocket engine
Fuel mass flow rate
Tunable diode laser absorption spectroscopy
Temperature
Partial pressure
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
作者:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
  |  
收藏
  |  
浏览/下载:32/0
  |  
提交时间:2020/05/18
Hybrid rocket engine
Paraffin-based fuel
Acrylonitrile-butadiene-styrene
Regression rate
Combustion efficiency
A 3D Numerical Study of LO2/GH(2) Supercritical Combustion in the ONERA-Mascotte Test-rig Configuration
期刊论文
OAI收割
2016
作者:
Benmansour, A., Liazid, A., Logerais, P. O. and Durastanti, J. F.
收藏
  |  
浏览/下载:38/0
  |  
提交时间:2017/05/27
Rocket engine non-premixed combustion supercritical regime H2-O2 flame transport properties large-eddy simulation flame stabilization cryogenic flames