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Right Angle Pipe with crude oil, inlet U of 1 meter per second, and outlet P of 0 Pa to compare against the Straight Pipe

Injectability of calciumphosphate suspensions

Parametric Optimization of Finned Heat Sinks

Trying to prove natural vventilation phenomena

Flow Analysis Over Alfa Romeo QV without any aerodynamic aids.

Experiments and comparaison of different single seater step planes at 180 km/h (50 m/s). I use a quickly made sort of single seater design.
Results :
Reference (no step plane)              : 1740 N of drag, 330 N of lift.
Flat step plane                                      : 1793 N of drag, 255 N of lift.
Flat step pland and side skirts     : 1800 N of drag, 55N of lift.
Flat step pland and all skirts         : 2025 N of drag, 650 N of lift.
Flat round step plane with skirt : 1880 N of drag, 760 N of downforce.
Angled step plane                               : 1840 N of drag, 450 N of downforce.
Angled step plane with skirts      : 1850 N of drag, 620 N of downforce.

Analysis of PTFE seated double offset buttefly valve design (150 class) In order to evaluate the Cv and pressure drop through valve.

Mon objectif est simuler un cyclone et avoir l'effet de la modification de sa géométrie sur l'efficacité de dépoussiérage

Calculating Cv for double offset butterfly valve

Straight Pipe with inlet U is 10 meters per s and outlet P is 0 Pa for the purposes of comparing to a Right Angle Pipe

this project is dedicated to investigating the drag effect on a special type of aircraft's tail, in order to test its aerodynamic efficiency.

This project investigates fluid-structure interaction between a wind turbine rotor and upstream wind

Examine the flow behaviour on train container body and calculate the drag force for different yaw angle.

To test the release of pressure from a vessel at different volumes at 630 bar to atmospheric pressure through a orifice. This is to relate the vessel volume to the time it takes for the vessel pressure to equal the atmospheric pressure.

Flow profile in a duct with different geometries

To study how will be the impact on housing when it falls from height

In this project incompressible fluid flow simulation of a conical draft tube is carried out. The parameters data is collected from the course book on fluid dynamics and the validation of CFD simulation result with the theoretical result is also performed. Steady state incompressible fluid flow simulation is selected for the given case.
The draft tube is a pipe of gradually increasing area, which connects the outlet of the water turbine's runner to the tail race. Draft tube helps to convert the exit velocity head into pressure or potential head.

The aim of the project was to implement a porous media option and try to understand the basic concept behind through CFD setup. for this case, incompressible flow simulation type was used. In this case, the pressure drop across the two was calculated and done some iteration.

A test project on how to get drag coefficients and center of pressure for a small submersible.

This simulation hopes to identify the increase in skin resistance of a racing shell with varying with boat speed and water line (depth of submersion) . The simulation is done for strictly horizontal motion not taking into consideration boat pitching and waves.

Essayons de modéliser un rond point et ses écoulements de flux

the intention of this project is to visualize the airflow inside of a cleanroom ISO4 and the influence of the equipment.                 Die Simulation zeigt ein Segment eines existierenden Reinraums der ISO-Klasse 4 aus den 1980er Jahren. Schon ohne Geraete ist die Luftstroemung weit vom Ideal, senkrechte, turbulenzarme Stroemung, laminar Flow, mit 0,45m pro s, entfernt ist.  Die Luftstroemung mit Equipment zeigt ein weiteres Projekt.

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