Hydrodynamic Instabilities Modeling in Hybrid Rocket Engines
Author:
Affiliation:
1. ONERA–The French Aerospace Lab, 31410 Mauzac, France
Funder
Région Occitanie
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34425
Reference24 articles.
1. Progress in Astronautics and Aeronautics Series;Karabeyoglu M. A.,2007
2. Progress in Astronautics and Aeronautics Series;Altman D.,2007
3. TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
4. Time-Resolved Fuel-Grain Port Diameter Measurement in Hybrid Rockets
5. An experimental investigation of pressure oscillations and their suppression in subscale hybrid rocket motors
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