Numerical Research on Mixing Combustion Characteristic of Vortex Flow Pancake Hybrid Rocket Motor

Author:

Zhang Zhiyuan,Liao Wenhe,Deng Hanyu,Cheng Yu,Xie Yongzhe,Hu Wenjun

Publisher

Elsevier BV

Reference32 articles.

1. Metal-organic frameworks as hypergolic additives for hybrid rockets;O Jobin;Chem Sci,2022

2. Three-dimensional numerical simulation of hybrid rocket motor based on dynamic mesh technology;X Meng;Aerosp. Sci. Technol,2023

3. Investigation of dynamic mixing combustion characteristics in variable thrust hybrid rocket motors;H Xia;Combust Flame,2023

4. Experimental and numerical investigation on thermochemical erosion and mechanical erosion of carbonbased nozzles in hybrid rocket motors;X Meng;Aerosp. Sci. Technol,2024

5. Three-dimensional printing of "Green" fuels for low-cost small spacecraft propulsion systems;S A Whitmore;J. Propuls. Power,2018

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