Aerodynamics

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F15 Fighter Jet

Inviscid flow over a fighter jet at transonic speed.

Computed with FluctSplit method.

Performed by TiagoQuintino and AndreaLani

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AGARD Wing

Fluid-Structure interaction of a transonic flow over a wing.

Flow computed with FiniteVolume method and structure computed with FiniteElement.

Performed by ThomasWuilbaut

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Dassault Falcon 50

Inviscid flow over a business jet at transonic speed.

Computed with FiniteVolume method.

Performed by AndreaLani

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ONERA M6 Wing

Transonic flow over the ONERA M6 wing. Computed with Fluctsplit.

Performed by TiagoQuintino

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Square cylinder

Subsonic compressible unsteady flow over a square cylinder at Reynolds 10000 and Mach 0.1

Computed with FiniteVolume method and LES using constant WALE model

Performed by WillemDeconinck

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