A modular particle-continuum numerical method for hypersonic non-equilibrium gas flows.
Thomas E. SchwartzentruberLeonardo C. ScalabrinIain D. BoydPublished in: J. Comput. Phys. (2007)
Keyphrases
- numerical methods
- runge kutta
- flow rate
- differential equations
- genetic algorithm
- partial differential equations
- boundary element method
- game theory
- nasa langley research center
- finite element method
- nash equilibrium
- numerical solution
- level set method
- finite difference method
- approximation schemes
- high order
- control system
- pairwise
- computational complexity
- pattern recognition
- similarity measure