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

detection of co2 level in computer lab using simulation

simulasi aliran udara terhadap panas heatsink

bulding construction in Oaxaca Mexico , seven levels

examen de un exagonal de análisis de elemento finito

Flow pas a bridge foundation with a square cross-section. RANS equations with k-epsilon turbulence model will be used.

Simulate flow characteristics of supersonic nozzle at sea level and 15 km above sea level

We are design a skyscraper for competition we need a wind load data of our design

Following the new 2021 F1 rules, this simulation showcases why is it really important to focus on diminishing the amount of dirty air that the following car is receiving when it comes to wheel-to-wheel battles.

Mixing different particles in a water tank.

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.

MED-T does not take credit for the structure and instruction for this simulation. Here, MED-T takes responsibility for relaying the information covered as faithfully and truthfully as possible. This simulation is credited to Milad Mafi. It was designed as part 3 of a three-part webinar project.

Webinar Project- Carotid Artery Bifurcation
The project simulates the flow of blood as a non-newtonian fluid through a realistic Carotid Artery Bifurcation. Simulations are performed for 3 cases- of a healthy blood vessel with no calcification or blockage and through a moderately and severely calcified or blocked a blood vessel. 
The results show the differences in pressure, velocity profile and the outlet flow through the 2 branches.

Flow conditions are based on a paper: STUDY OF BLOOD FLOW IN A BIFURCATION WITH A STENOSIS,
Sonia I.S. Pinto, E.D. Costa, J.B.L.M. Campos, J.M. Miranda

Simulation of air conditioning currents in an office, with curtain wall, with and without UV adhesive sun protection

The project goal was to find the best airflow around the operation theatre with a different Duct model.
so to achieve this goal, the duct was simulated with incompressible flow simulation type and then operation room was simulated with convection heat transfer simulation type.
At the end, The results of both duct design were compared and find the optimum duct design with respect to the operation room.

The project simulates the flow of water through an orifice. The water is assumed to be incompressible and the k-omega SST turbulence model is used as the large pipe diameter and inlet velocity of 2 m/s is likely to result in a turbulent flow  and so using a laminar flow model would lead to incorrect results. It is possible to calculate the degree of turbulence via the Reynolds number. The results show that a jet forms after the orifice,  and the water attains a maximum velocity of 5.9 m/s. The orifice causes a low pressure region to form directly after the orifice. The pressure in the low pressure region falls to below the pressure and the outlet of the pipe. The jet leaving the orifice drives a toroid shaped vortex around the edges of the pipe. In the vortex region, the flow recirculates with minimal exchange of liquid. The orifice causes a large pressure drop, much larger than would occur if the entire length of pipe were of the diameters of the orifice.

DETERMINE ENERGY LOSSES IN A CLOSED LOOP PIPE

flow simulation | SimScale Project Library | Page 4