Numerical and experimental investigations on injection effects of orifice injector plate in hybrid rocket motors
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference21 articles.
1. Numerical simulation of liquid droplet breakup in supersonic flows;Liu;Acta Astronaut.,2018
2. Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain;Tian;Acta Astronaut.,2014
3. Thrust control by fluidic injection in solid rocket motors;Guo;J. Propul. Power,2017
4. One-dimensional theoretical analysis of dilute particle-gas swirling flow in the laval nozzle;Guo;AIAA J.,2018
5. Mixing augmentation of transverse hydrogen jet by injection of micro air jets in supersonic crossflow;Anazadehsayed;Acta Astronaut.,2017
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