Three-dimensional numerical analysis on combustion performance and flow of hybrid rocket motor with multi-segmented grain
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference21 articles.
1. Hybrid uncertainty-based design optimization and its application to hybrid rocket motors for manned lunar landing;Zhu;Chin J Aeronaut,2017
2. Uncertainty analysis and design optimization of hybrid rocket motor powered vehicle for suborbital flight;Zhu;Chin J Aeronaut,2015
3. Transient simulation of regression rate on thrust regulation process in hybrid rocket motor;Tian;Chin J Aeronaut,2014
4. Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection;Li;Acta Astronaut,2016
5. Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain;Tian;Acta Astronaut,2014
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