Simulation of Surface Instabilities in Liquefying Hybrid Rocket Fuels
Author:
Affiliation:
1. Pennsylvania State University
Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. Theoretical and experimental analysis of liquid layer instability in hybrid rocket engines
2. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
3. Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines
4. Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors
5. Scale-Up Tests of High Regression Rate Paraffin-Based Hybrid Rocket Fuels
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2. Simulation of Liquefying Propellants in Cross-Flow Configurations;AIAA AVIATION 2022 Forum;2022-06-20
3. Self-consistent surface-temperature boundary condition for liquefying-fuel-based hybrid rockets internal-ballistics simulation;International Journal of Heat and Mass Transfer;2021-04
4. Increasing Undergraduate Involvement in Propulsion at Penn State Harrisburg;AIAA Propulsion and Energy 2019 Forum;2019-08-16
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