CFD Simulations of Self-pressurized Nitrous Oxide Hybrid Rocket Motors
Author:
Affiliation:
1. University of Padova
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4534
Reference29 articles.
1. Integrated approach for hybrid rocket technology development
2. Numerical Investigation of the Effect of a Diaphragm on the Performance of a Hybrid Rocket Motor
3. CFD Simulation of a Hybrid Rocket Motor with Liquid Injection
4. Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales
5. Testing and CFD Simulation of Diaphragm Hybrid Rocket Motors
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