Numerical analysis of LOx-BioLPG combustion in high-pressure liquid rocket engine propulsion system

Author:

Islam Md.RhyhanulORCID,Ahmed Zahir U.,Hossain Khandkar Aftab

Publisher

Elsevier BV

Subject

Filtration and Separation,Fluid Flow and Transfer Processes,Process Chemistry and Technology,Energy (miscellaneous),Education,Catalysis

Reference68 articles.

1. Renewable and tuneable bio-LPG blends derived from amino acids;Amer;Biotechnol. Biofuels.,2020

2. Global combustion mechanisms for use in CFD modeling under oxy-fuel conditions;Andersen;Energy & Fuels.,2009

3. Fundamentals of Aerodynamics;Anderson,2010

4. The HYPROB demonstrator line: status of the LOX/LCH4 propulsion activities;Battista,2019

5. A 3D numerical study of LO2/GH2 supercritical combustion in the ONERA-Mascotte Test-rig configuration;Benmansour;J. Therm. Sci.,2016

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Impact of BioLPG’s on Carbon Footprint: A Context of European Countries;Liquefied Petroleum Gas - Recent Advances and Technologies for Energy Transition [Working Title];2024-02-01

2. Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets;Aerospace;2023-08-28

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