CFD Simulation of a 1kN Paraffin-fueled Hybrid Rocket Engine
Author:
Affiliation:
1. Royal Military Academy
2. Université Libre de Bruxelles
Publisher
American Institute of Aeronautics and Astronautics
Reference35 articles.
1. Sutton, G. P., and Biblarz, O., Rocket Propulsion Elements, 9thed.2017, pp.5-9.
2. Development and testing of paraffin-based hybrid rocket fuels
3. State of Art and Current Challenges of the Paraffin-Based Hybrid Rocket Technology
4. Computational Methods for Fluid Dynamics
Cited by 3 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. Computational Fluid Dynamics Analysis of Flow Field of Different Hybrid Rocket Engine Oxidizer Injector Designs;AIAA SCITECH 2024 Forum;2024-01-04
2. Numerical Investigation of the Geometrical Design of a 1kN Paraffin-Fueled Hybrid Rocket Motor;AIAA SCITECH 2022 Forum;2022-01-03
3. Two-Phase CFD Simulation of a 1kN Paraffin-Fueled Hybrid Rocket Motor;AIAA Propulsion and Energy 2021 Forum;2021-07-28
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