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Hassan Hourie

Turbo-Fan CAD/CFD model
A concept mixing nozzle was designed with the objective of introducing optical blockage to the engine's turbine blades.
![1[89].PNG](https://static.wixstatic.com/media/80a37d_efa9ed14c1734919acd0c2bb114ca0a3~mv2.png/v1/fill/w_378,h_283,al_c,q_85,usm_0.66_1.00_0.01,enc_avif,quality_auto/1%5B89%5D_PNG.png)
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
![2[97].PNG](https://static.wixstatic.com/media/80a37d_95a494ec05e4409683c23d486d15f5b2~mv2.png/v1/fill/w_402,h_283,al_c,q_85,usm_0.66_1.00_0.01,enc_avif,quality_auto/2%5B97%5D_PNG.png)

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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