Predictive CFD Model for Internal Ballistics of Hybrid Rocket Engines using Supercritical Paraffin-wax and Oxygen
Author:
Affiliation:
1. University of Rome "La Sapienza"
Publisher
American Institute of Aeronautics and Astronautics
Reference44 articles.
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Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Numerical Simulations of the Internal Ballistics of Paraffin–Oxygen Hybrid Rockets at Different Scales;Aerospace;2021-08-05
2. Self-consistent surface-temperature boundary condition for liquefying-fuel-based hybrid rockets internal-ballistics simulation;International Journal of Heat and Mass Transfer;2021-04
3. Prediction of Space and Time Distribution of Wax-based Fuel Regression Rate in a Hybrid Rocket;AIAA Propulsion and Energy 2020 Forum;2020-08-17
4. Combustion Efficiency in Single Port Hybrid Rocket Engines;AIAA Propulsion and Energy 2020 Forum;2020-08-17
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