Experimental Investigation on Combustion Characteristics of Hybrid Rocket Fuels with Multi-Angle Diverging Injector
Injection pattern of the oxidizer injected into the combustion chamber is a significant factor in evaluating the performance of a hybrid rocket. In the hybrid rocket combustion process, oxidizer flows over the solid fuel grain surface, leading to a turbulent diffusion boundary layer formation and th...
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| פורמט: | Article |
| שפה: | English |
| יצא לאור: |
MDPI AG
2020-06-01
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| סדרה: | International Journal of Turbomachinery, Propulsion and Power |
| נושאים: | |
| גישה מקוונת: | https://www.mdpi.com/2504-186X/5/2/12 |