Airbus Aircraft

This is a Navier Stokes calculation using an 8 million point mesh of an Airbus type aircraft. The image shows the pressure distribution.

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UCAV

Steady-state Euler simulation of a UCAV at a Mach number of 0.22 and an angle of attack of 15 degrees.

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Porsche 911

Euler flow solution computed with Edge, simulating the airflow round a Porsche 911.

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Twin-Engine Aircraft

An Euler simulation of a generic twin-engine aircraft.

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RAE M2129 S-duct

RAE M2129 S-duct to reduce flow separation at inlet Mach number M=0.66, Reynolds number 0.39 million.

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