Chemical behavior research of high-energy aerospace propellant with a mesoscale heterogeneous packing model

Author:

Chen Kaixuan,Ye Zhenwei,Xue Xiaochun,Yu Yonggang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference34 articles.

1. Insight into graphene-salen metal nanocomposites on combustion performance and mechanism of HMX-CMDB propellant;Zhang;Chem. Eng. J.,2022

2. Microwave controlled ignition and combustion characteristics of ADN-based ionic liquid propellant with fast response and environmental friendliness;Cheng;Chem. Eng. J.,2023

3. Directional combustion induced by 3D aligned carbon channel arrays for combustion chamber-free micro-thruster;Tang;Chem. Eng. J.,2022

4. Recent progress in modeling solid propellant combustion[J];Beckstead;Combust Explo Shock+.,2006

5. Modeling of heterogeneous propellant combustion: a survey;Jackson;AIAA J.,2012

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