Simulation of the Condensed Phase Particles Electrization in Combustion Products of the Model Hybrid Rocket Engine
Author:
Affiliation:
1. Bauman Moscow State Technical University,Moscow,Russian Federation
Funder
Rocket
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10086702/10086686/10086842.pdf?arnumber=10086842
Reference25 articles.
1. Formation Mechanism Analysis and Detection of Charged Particles in an Aero-engine Gas Path
2. Mathematical simulation of the condensed phase particles electrization in high-temperature flow of the rocket engine combustion products;rudinsky;TVT – TPhHT,2019
3. The design and control of a labscale hybrid rocket facility for spectroscopy studies
4. Analytical and Numerical Investigations into Hemisphere-Shaped Electrostatic Sensors
5. Ionized gas flow magnetic field as the diagnostic parameter in LRE testing and operation;pushkin;Technical Information Bull,2015
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