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High order methods for aeronautics & aeroacoustics

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andrealani edited this page Sep 29, 2014 · 1 revision

NACA 1

Simulated pressure coefficient on NASA airfoil with 2nd-, 3rd- and 4th-order Residual Distribution Schemes by M. Vymazal.

![Subsonic flow over cylinder] (https://github.com/andrealani/COOLFluiD/blob/master/pics/cylinder_re40_sfd_p2p3.png)

Simulation of subsonic flow over cylinder with 4th-order Spectral Finite DIfference by K. Vanden Abeele.

The COOLFluiD team is involved and open to new collaborations in Horizon2020, ESA and other research projects dealing with complex multi-disciplinary problems and computational challenges.

Training sessions and consulting services can also be provided on demand.

For any request or suggestions please contact [email protected]

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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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