Numerical simulation of chemical ablation and mechanical erosion in hybrid rocket nozzle
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference20 articles.
1. Chemical erosion of carbon-carbon/graphite nozzles in solid-propellant rocket motors;Thakre;J. Propul. Power,2008
2. Numerical analysis of nozzle material thermochemical erosion in hybrid rocket engines;Bianchi;J. Propul. Power,2013
3. Numerical and experimental study of the thermochemical erosion of a graphite nozzle in a hybrid rocket motor with a star grain;Hui;Acta Astronaut.,2019
4. Comparison of ablative materials in a simulated solid rocket exhaust environment;Koo,1991
5. Mechanical erosion of graphite nozzle in solid-propellant rocket motor;Thakre;J. Propul. Power,2013
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