Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket-Reference-Cited by-同舟云学术

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Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket

Published:2019-06 Issue: Volume:89 Page:431-444
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Di Martino G.D.^ORCID,Mungiguerra S.,Carmicino C.,Savino R.

Funder

MIUR

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Hybrid rocket propulsion systems;Altman,1995

2. Experimental investigation into the effect of solid-fuel additives on hybrid rocket performance;Carmicino;J. Propuls. Power,2015

3. Overview and history of hybrid rocket propulsion;Altman,2007

4. New perspectives for hybrid propulsion;Oikine,2006

5. Nammo hybrid rocket propulsion TRL improvement program;Ronningen,2012

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1. On the Multidisciplinary Design of a Hybrid Rocket Launcher with a Composite Overwrapped Pressure Vessel;Journal of Composites Science;2024-03-19

2. Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate;International Journal of Heat and Mass Transfer;2024-03

3. Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels;AIAA Journal;2023-08

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5. Numerical study of the effect of fuel droplets on the combustion proceeding under typical conditions of hybrid rocket engines;Thermophysics and Aeromechanics;2023-06-05

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