Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 2: Comparison
Author:
Affiliation:
1. Pusan National University, Pusan 609-735, Republic of Korea
2. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1087
Reference22 articles.
1. Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 1: Validation
2. Computation of unsteady shock-induced combustion using logarithmic species conservation equations
3. Flow features of shock-induced combustion around projectile traveling at hypervelocities
4. Simulation of shock-induced combustion past blunt projectiles using shock-fitting technique
5. A fully implicit time accurate method for hypersonic combustion - Application to shock-induced combustion instability
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