Ignition delay and low-frequency coupling in hybrid rocket combustion
Author:
Funder
National Research Foundation of Korea
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference23 articles.
1. Vortex shedding influence on hybrid rocket pressure oscillations and combustion efficiency;Messineo;J. Propul. Power,2016
2. Passive control of low-frequency instability in hybrid rocket combustion;Hyun;Aerospace,2021
3. Low frequency instability in laboratory-scale hybrid rocket motors;Park;Aero. Sci. Technol.,2015
4. Modeling of hybrid rocket low frequency instabilities;Karabeyoglu;J. Propul. Power,2005
5. Thermal Transients in the Hybrid Rocket Fuel Grains - Nonlinear Effects;Karabeyoglu,2007
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. Numerical and experimental investigations of micro Al particle additive on the performances of HTPB hybrid rocket motors;Acta Astronautica;2024-07
2. Long-Duration Dynamic Numerical Simulation of Combustion and Flow in Hybrid Rocket Motors Considering Nozzle Erosion;Aerospace;2024-04-18
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