Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales
Author:
Affiliation:
1. Interdepartmental Center for Space Studies and Activities (CISAS), University of Padua, 35131 Padova, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35528
Reference13 articles.
1. Navier-Stokes Investigation on Reacting Flow Field of HTPB/O2 Hybrid Motor and Regression Rate Evaluation
2. A Physics Based Comprehensive Mathematical Model to Predict Motor Performance in Hybrid Rocket Propulsion Systems
3. Simulation Code for Hybrid Rocket Combustion
4. 2D transient numerical code for hybrid rocket simulations with detailed chemistry
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