Three-dimensional numerical analysis on combustion performance and flow of hybrid rocket motor with multi-segmented grain

Chinese Journal of Aeronautics ◽

10.1016/j.cja.2019.12.021 ◽

2020 ◽

Vol 33 (4) ◽

pp. 1181-1191 ◽

Author(s):

Hui TIAN ◽

Yu DUAN ◽

Hao ZHU

Keyword(s):

Numerical Analysis ◽

Three Dimensional ◽

Rocket Motor ◽

Hybrid Rocket ◽

Combustion Performance ◽

Hybrid Rocket Motor

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Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor

Acta Astronautica ◽

10.1016/j.actaastro.2017.08.022 ◽

2017 ◽

Vol 140 ◽

pp. 247-254 ◽

Author(s):

Hui Tian ◽

Ruipeng Yu ◽

Hao Zhu ◽

Junfeng Wu ◽

Guobiao Cai

Keyword(s):

Experimental Studies ◽

Three Dimensional ◽

Rocket Motor ◽

Hybrid Rocket ◽

Hybrid Rocket Motor

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Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection

Acta Astronautica ◽

10.1016/j.actaastro.2016.02.023 ◽

2016 ◽

Vol 123 ◽

pp. 26-36 ◽

Author(s):

Chengen Li ◽

Guobiao Cai ◽

Hui Tian

Keyword(s):

Numerical Analysis ◽

Combustion Characteristics ◽

Rocket Motor ◽

Hybrid Rocket ◽

Hybrid Rocket Motor

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Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulation

Aerospace Science and Technology ◽

10.1016/j.ast.2015.01.014 ◽

2015 ◽

Vol 42 ◽

pp. 287-296 ◽

Author(s):

Xingliang Sun ◽

Hui Tian ◽

Nanjia Yu ◽

Guobiao Cai

Keyword(s):

Numerical Simulation ◽

Rocket Motor ◽

Hybrid Rocket ◽

Regression Rate ◽

Combustion Performance ◽

Hybrid Rocket Motor

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Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number

Aerospace Science and Technology ◽

10.1016/j.ast.2020.105922 ◽

2020 ◽

Vol 103 ◽

pp. 105922 ◽

Author(s):

Guobiao Cai ◽

Zeng Zhao ◽

Bo Zhao ◽

Yufei Liu ◽

Nanjia Yu

Keyword(s):

Rocket Motor ◽

Hybrid Rocket ◽

Swirl Number ◽

Regression Rate ◽

Combustion Performance ◽

Hybrid Rocket Motor

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Numerical analysis of the hybrid rocket motor with axial injection based on oxidizer flow distribution

Acta Astronautica ◽

10.1016/j.actaastro.2021.12.025 ◽

2021 ◽

Author(s):

Hui Tian ◽

Xianzhu Jiang ◽

Hao Zhu ◽

Ruipeng Yu ◽

Yuanjun Zhang ◽

...

Keyword(s):

Numerical Analysis ◽

Flow Distribution ◽

Rocket Motor ◽

Hybrid Rocket ◽

Axial Injection ◽

Hybrid Rocket Motor

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Combustion performance and scale effect from N2O/HTPB hybrid rocket motor simulations

Acta Astronautica ◽

10.1016/j.actaastro.2012.12.013 ◽

2013 ◽

Vol 85 ◽

pp. 1-11 ◽

Author(s):

Fanli Shan ◽

Lingyun Hou ◽

Ying Piao

Keyword(s):

Scale Effect ◽

Rocket Motor ◽

Hybrid Rocket ◽

Combustion Performance ◽

Hybrid Rocket Motor

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Parametric investigation of secondary injection in post-chamber on combustion performance for hybrid rocket motor

Acta Astronautica ◽

10.1016/j.actaastro.2017.09.009 ◽

2017 ◽

Vol 140 ◽

pp. 427-438 ◽

Author(s):

Guobiao Cai ◽

Binbin Cao ◽

Hao Zhu ◽

Hui Tian ◽

Xuan Ma

Keyword(s):

Rocket Motor ◽

Hybrid Rocket ◽

Parametric Investigation ◽

Combustion Performance ◽

Hybrid Rocket Motor ◽

Secondary Injection

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Development and Three-dimensional Numerical Simulation of a Double-tube Hybrid Rocket Motor

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2014-3546 ◽

2014 ◽

Author(s):

Arnau Pons Lorente ◽

Nanjia Yu ◽

Peng Zeng ◽

Bo Zhao

Keyword(s):

Numerical Simulation ◽

Three Dimensional ◽

Rocket Motor ◽

Hybrid Rocket ◽

Hybrid Rocket Motor

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Combustion Performance of Hybrid Rocket Motor Under the Influence of Cylindrical Protrusion

Advances in Applied Mechanical Engineering - Lecture Notes in Mechanical Engineering ◽

10.1007/978-981-15-1201-8_2 ◽

2020 ◽

pp. 11-18

Author(s):

Kabaleeswaran Manikandan ◽

K. Lakshmi Das ◽

N. Purushothaman ◽

L. Karthik

Keyword(s):

Rocket Motor ◽

Hybrid Rocket ◽

Combustion Performance ◽

Hybrid Rocket Motor ◽

Cylindrical Protrusion

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Quasi 1-D Numerical Analysis of Combustion Instability in Hybrid Rocket Motor Incorporating Boundary Layer Lags

52nd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2016-4751 ◽

2016 ◽

Author(s):

Goutham Karthikeyan ◽

Toru Shimada

Keyword(s):

Boundary Layer ◽

Numerical Analysis ◽

Combustion Instability ◽

Rocket Motor ◽

Hybrid Rocket ◽

Hybrid Rocket Motor

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