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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties
期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
作者:
Wang, Ruoyan
;
Lin, Xin
;
Wang, Zezhong
;
Wu, Kun
;
Pan, Junjie
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浏览/下载:0/0
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提交时间:2024/05/21
Hybrid rocket
Composite fuel grain
Characteristic structure
Radiation image
Combustion properties
Experimental Study on Supersonic Combustion Characteristics of Al/B-Kerosene Nanofuels
期刊论文
AIAA JOURNAL, 2024, 页码: 9
作者:
Fan, Wenhui
;
Zhong, Fengquan
;
Gao, Zhanbiao
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浏览/下载:0/0
  |  
提交时间:2024/05/21
Plasma Assisted Combustion
Petroleum
Nanomaterials
Supersonic Combustor
Flow Measurement
Optical Properties
Boundary Layers
Hydrocarbon Fuels
Band Pass Filter
Heat and Mass Transfer
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine
期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9
作者:
Wang, Zezhong
;
Lin, Xin
;
Pan, Junjie
;
Luo, Jiaxiao
;
Wang, Ruoyan
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  |  
浏览/下载:50/0
  |  
提交时间:2024/05/21
Combustion Efficiency
Emission Spectroscopy
Hybrid Rocket Engines
Paraffin Based Fuels
Regression rate
Aluminium Alloys
3D Printing
Experimental investigation of mode transition process in a cavity-based scramjet
期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11
作者:
Meng, Yu
;
Sun, Wenming
;
Gu, Hongbin
;
Chen, Fang
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  |  
浏览/下载:1/0
  |  
提交时间:2024/05/14
Turbulent burning velocity of NH3/H2/air mixtures spherical flames: Effects of differential diffusion and turbulent stretch
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 卷号: 59, 页码: 525-534
作者:
Cao, JianBin
;
Zhao, Nan Nan
;
Li, GuoXiu
;
Li, HongMeng
;
Zhang GP(张国鹏)
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浏览/下载:2/0
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提交时间:2024/04/29
Ammonia/hydrogen/air mixtures
Turbulent expending flame
Differential diffusion
Turbulent stretch
Turbulent burning velocity
Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications
期刊论文
APPLIED THERMAL ENGINEERING, 2024, 卷号: 238, 页码: 15
作者:
Gao EK(高尔康)
;
Zhong FQ(仲峰泉)
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提交时间:2024/02/26
Direct thermoelectric conversion
Regenerative cooling
Supersonic combustor
Analytical model
Genetic algorithm
On the transition modes and mechanisms for laminar to turbulent lifted jet diffusion flames at normal- and micro-gravity
期刊论文
COMBUSTION AND FLAME, 2024, 卷号: 260, 页码: 10
作者:
Li D(李丹)
;
Wen, Yuzhe
;
Liu, Yu Cheng
;
Wang SF(王双峰)
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提交时间:2024/02/26
Lifted flame
Non-premixed jet
Transition to turbulence
Flame stability
Microgravity
Influence of non-thermal plasma and electric field on non-premixed methane flame
期刊论文
THERMAL SCIENCE AND ENGINEERING PROGRESS, 2024, 卷号: 47, 页码: 15
作者:
Zhang YF(张玉锋)
;
Li T(李腾)
;
Wei XL(魏小林)
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  |  
浏览/下载:1/0
  |  
提交时间:2024/03/11
Non -thermal plasma
Coaxial micro -tube burner
Methane flame
Combustion stability
Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
期刊论文
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:173/0
  |  
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
>
Effect of droplet diameter on oblique detonations with partially pre-vaporized n-heptane sprays
期刊论文
COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 12
作者:
Teng, Honghui
;
Tian, Cheng
;
Yang, Pengfei
;
Zhao, Majie
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  |  
浏览/下载:13/0
  |  
提交时间:2023/11/28
Liquid ODWs
Partially pre-vaporized
Eulerian-Lagrangian method
Droplet diameter
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