Boundary layer combustion of paraffin fuels for hybrid propulsion applications
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference26 articles.
1. Three-dimensional numerical modeling of a rocket engine with solid fuel;Kushnirenko;Acta Astronaut.,2021
2. Low cost small-satellite access to space using hybrid rocket propulsion;Schmierer;Acta Astronaut.,2019
3. Numerical investigations of hybrid rocket engines[J];Betelin;Acta Astronaut.,2018
4. Numerical simulation of low-melting temperature solid fuel regression in hybrid rocket engines[J];Rashkovskiy;Acta Astronaut.,2020
5. Experimental study of severity level of structural discontinuities in paraffin grains of hybrid propellant rocket[J];Andrianov;Acta Astronaut.,2019
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1. Surface Structure of Reacting Solid Ramjet Fuels;Journal of Propulsion and Power;2024-05
2. The effect of coupled combustion reaction on conjugate heat transfer in boundary layer of a segregated oxidizer/fuel solid motor;International Journal of Thermal Sciences;2023-11
3. Model for Combustion Instability in Hybrid Rocket Engines Burning Liquefying Fuels;AIAA Journal;2023-08
4. Droplet entrainment and its role in the combustion of HTPB/paraffin fuels;Acta Astronautica;2023-03
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