Modelling of hybrid rocket flow-fields with computational fluid dynamics
A low regression rate is a major limitation in the hybrid rocket propulsion system. This paper is to study the regression rate characteristics of a cylindrical solid grain with cryogenic propellants. Paraffin (P) fuel is coupled with two types of oxidizers, namely gaseous...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | en |
| Published: |
Semarak Ilmu Publishing
2022
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/97449/7/97449_Modelling%20of%20hybrid%20rocket%20flow-fields.pdf http://irep.iium.edu.my/97449/ https://semarakilmu.com.my/journals/index.php/CFD_Letters/article/view/461/229 https://doi.org/10.37934/cfdl.14.3.5367 |
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