An Analytical Model to Predict Longitudinal Acoustic Modes Frequency of Hybrid Rockets Combustion Chamber
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/10.2514/6.2017-4645
Reference19 articles.
1. An experimental investigation of pressure oscillations and their suppression in subscale hybrid rocket motors
2. Experimental investigation of labscale hybrid instability
3. Combustion Oscillations in High Regression Rate Hybrid Rockets
4. Modeling of Hybrid Rocket Low Frequency Instabilities
5. Combustion instability related to vortex shedding in dump combustors and their passive control
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2. Spatial Temporal Modeling of a Hybrid Rocket to Study Low Frequency Combustion Instabilities;AIAA Propulsion and Energy 2020 Forum;2020-08-17
3. Transient Generalized Two Temperatures Approach to Model the Non-acoustic Combustion Instability of a Hybrid Rocket;AIAA Propulsion and Energy 2020 Forum;2020-08-17
4. CFD Modeling of a Hybrid Rocket Using a Generalized One-dimensional Model of the Flame Temperature;AIAA Propulsion and Energy 2019 Forum;2019-08-16
5. LF and HF Combustion Instability in Hybrid Rocket Engines;2018 Joint Propulsion Conference;2018-07-08
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