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Source Publication:ACTA ASTRONAUTICA
Community:高温气体动力学国家重点实验室
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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
Authors:
Wang, Ruoyan
;
Lin, Xin
;
Wang, Zezhong
;
Wu, Kun
;
Pan, Junjie
;
Zhang, Zelin
;
Luo, Jiaxiao
;
Li, Fei
;
Yu, Xilong
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View/Download:4/0
  |  
Submit date:2024/05/21
Hybrid rocket
Composite fuel grain
Characteristic structure
Radiation image
Combustion properties
Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295
Authors:
Ao Y(敖彧)
;
Wu K(吴坤)
;
Lu, Hongbo
;
Ji, Feng
;
Fan XJ(范学军)
Adobe PDF(11339Kb)
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View/Download:96/5
  |  
Submit date:2023/06/15
Hypervelocity combustion
Thermal nonequilibrium
Two-temperature model
Numerical simulation
An experimental investigation of supersonic combustion of cracked JP-10
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 203, 页码: 329-340
Authors:
Cui NF(崔乃夫)
;
Rao W(饶威)
;
Li YJ(李昱君)
;
Zhu, Yinhai
;
Zhang TC(张泰昌)
;
Fan XJ(范学军)
Adobe PDF(14542Kb)
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View/Download:138/5
  |  
Submit date:2023/02/07
Cracking
JP-10
Supersonic combustion
Regenerative cooling
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion
期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:
Xue R
;
Zheng X
;
Yue LJ(岳连捷)
;
Zhang SK
;
Weng C
Adobe PDF(3912Kb)
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View/Download:345/234
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Submit date:2020/08/26
Compressible boundary layer combustion
Skin-friction reduction
Boundary layer transition
Transition k-kl-w model
Hydrogen combustion