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Turbo-Fan CAD/CFD model

A concept mixing nozzle was designed with the objective of introducing optical blockage to the engine's turbine blades. 

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01

Baseline Engine CAD model

The nacelle and core engine are shown 

02

Baseline Engine with the concept mixing nozzle

Nacelle, core engine and mixing nozzle are shown

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03

One lobe from the mixing nozzle

Here you can see the swirl bend in one of the mixing nozzle lobes

04

Engine with four temperature counters downstream of the nozzle

RANS CFD simulation results. Engine with four temperature contours. 

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