On the Explanation of the “DC Shift” in Hybrid Rockets
Author:
Affiliation:
1. University of Naples "Federico II"
2. Technical University of Turin
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4525
Reference18 articles.
1. Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift
2. Modeling of Hybrid Rocket Low Frequency Instabilities
3. Acoustics, Vortex Shedding, and Low-Frequency Dynamics Interaction in an Unstable Hybrid Rocket
4. Dynamic Modeling of Hybrid Rocket Combustion
5. Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors
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1. Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines;Journal of Spacecraft and Rockets;2024-05
2. Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities;AIAA SCITECH 2024 Forum;2024-01-04
3. Multiphysics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability;AIAA AVIATION 2022 Forum;2022-06-20
4. Effect of Protrusion on Combustion Stability of Hybrid Rocket Motor;Propellants, Explosives, Pyrotechnics;2022-03-09
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