Multi-disciplinary modeling of injection, mixing and combustion in liquid rocket engines
cun id:
1757
PROPULSIONE AEROSPAZIALE
Development of numerical methods for the analysis of three-dimensional shock/boundary layer interactions
Parallel computing server for numerical characterization of space transportation vehicles
Combined RANS/DNS analysis of conjugate heat transfer in rocket cooling channels
Numerical and experimental investigation of biopolymers -based hybrid propulsion
Numerical generation of flamelet databases for multidimensional reactive flows using an algorithm for multi-scale adaptive model reduction and a parallel adaptive wavelet method
Numerical study on transverse combustion instability in liquid propellant rocket engines for the achievement of predictive capability using a simplified model
Multi-fidelity numerical investigation of transcritical combustion and heat transfer in Liquid Rocket Engine propulsion systems
Advanced modeling of reactive flows in next generation throttleable, restartable liquid-propellant rocket engine.
Development of new numerical techniques based on shock-fitting for the simulation of viscous flows with shock waves.