Regression Modeling of Paraffin-based Hybrid Rocket Fuels for Internal Ballistics Simulation
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American Institute of Aeronautics and Astronautics
Reference10 articles.
1. Scale-up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels
2. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
3. Combustion of Liquefying Hybrid Propellants: Part 2, Stability of Liquid Films
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. State of Art and Current Challenges of the Paraffin-Based Hybrid Rocket Technology;AIAA Propulsion and Energy 2019 Forum;2019-08-16
2. Modeling of gas–surface interface for paraffin-based hybrid rocket fuels in computational fluid dynamics simulations;Progress in Propulsion Physics – Volume 11;2019
3. Flowfield Calculation Coupled with Fuel Surface Regression in Combustion Chamber for Swirling-Oxidizer-Type Hybrid Rocket Engine;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
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