2D transient numerical code for hybrid rocket simulations with detailed chemistry
Author:
Affiliation:
1. University of Orléans
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3212
Reference34 articles.
1. Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines
2. Development of a small sounding hybrid rocket with a swirling-oxidizer-type engine
3. Characterization of Fuel Regression in a Radial Flow Hybrid Rocket
4. Scale-up Tests of High Regression Rate Liquefying Hybrid Rocket Fuels
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3. Methodologies for Detailed Chemistry Computation, Application to Hybrid Rocket Combustion Chamber Simulations;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12
4. Micro and Full-Scale Experiments on Hybrid Rocket Fuel and Prelude to Hybrid Rocket Combustor Simulations;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12
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