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Reentry aerothermodynamics

Andrea Lani edited this page Nov 7, 2016 · 1 revision

Mach number field for ESA BLAST capsule (M=15, two-temperature model)

Mach number field for ESA BLAST capsule (M=15, two-temperature model) by A. Lani.


Mach and vibrational temperature fields for ESA EXPERT simulation at M=13.5

Mach and vibrational temperature fields for ESA EXPERT simulation (M=13.5) by A. Lani.


Collisional radiative models

Electronic energy populations for atomic nitrogen predicted by a pioneering 2D axial-symmetric simulation using reduced collisional-radiative models at 1.0 cm from the shock front in Fire II case at 1634 s. More details on the computational model are available here.

Contacts

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HOWTO

2019 NASA Ames presentation

2014 NASA Ames presentation


parallel computations of complex problems

Parallel mesh decomposition


Scalability in large scale simulation

High-performance computing (strong scaling on NASA Pleiades for 1/2 billion-cells 3D grid)


Modeling of high-speed reacting flows and plasma

Chemically reacting flows and plasma


Numerical Schlieren of turbulent flow on wing computed with RDS-LES

Complex all-speed flow simulations

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