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...

Full description

Bibliographic Details

Main Authors:	Ismail, Izham Izzat, Rozainuddin, Nur Husnina Aufa, Nordin, Norhuda Hidayah, Azami, Muhammad Hanafi
Format:	Article
Language:	en
Published:	Semarak Ilmu Publishing 2022
Subjects:	TL780 Rockets TL787 Astronautics
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
Tags:	Add Tag No Tags, Be the first to tag this record!