PROPULSIONE AEROSPAZIALE | Ricerc@Sapienza

PROPULSIONE AEROSPAZIALE

cun id:

1757

Multi-disciplinary modeling of injection, mixing and combustion in liquid rocket engines

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 10:24

Development of numerical methods for the analysis of three-dimensional shock/boundary layer interactions

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 10:20

Parallel computing server for numerical characterization of space transportation vehicles

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 10:10

Combined RANS/DNS analysis of conjugate heat transfer in rocket cooling channels

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 07:30

Numerical and experimental investigation of biopolymers -based hybrid propulsion

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 07:26

Numerical generation of flamelet databases for multidimensional reactive flows using an algorithm for multi-scale adaptive model reduction and a parallel adaptive wavelet method

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 07:19

Numerical study on transverse combustion instability in liquid propellant rocket engines for the achievement of predictive capability using a simplified model

Submitted by Anonimo (not verified) on Tue, 19/04/2022 - 07:14

Multi-fidelity numerical investigation of transcritical combustion and heat transfer in Liquid Rocket Engine propulsion systems

Submitted by Anonimo (not verified) on Wed, 13/04/2022 - 12:37

Advanced modeling of reactive flows in next generation throttleable, restartable liquid-propellant rocket engine.

Submitted by Anonimo (not verified) on Wed, 13/04/2022 - 12:34

Development of new numerical techniques based on shock-fitting for the simulation of viscous flows with shock waves.

Submitted by Anonimo (not verified) on Wed, 13/04/2022 - 12:28

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