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This project investigates the dynamic interaction of a high-pressure water jet with a perforated sheet, focusing on the fluid flow characteristics and sound pattern generation. The study explores the role of irregular perforation geometry in influencing pressure distribution, flow patterns, and acoustic propagation. The simulation employs Computational Fluid Dynamics (CFD) to analyze:
Velocity and pressure fields around perforations.
Turbulence and vortex formation due to irregular geometries.
Acoustic wave propagation resulting from fluid-solid interaction.

estudo de fluxos em espaços construídos

This project aims to investigate the potential for room-temperature superconductivity using germanium quantum dots. The experimental methods and procedure section outlines the steps taken to conduct the experiment, as well as the data collected, including the sample size, temperature, applied voltage, measured current, and resistance of the sample at each temperature.

The goal of the project is to optimize the design of an F1 Rear wing. An incompressible flow simulation will be used with a speed of 10m/s (36km/h) at the inlet and on the floor. 

F1 Rear wings are designed to create more negative lift on the car by deflecting the incoming air and creating flow separation. This serves to reduce the amount of drag experienced by the vehicle which allows to it move faster in a given distance than a vehicle that doesn't possess one. 

Feel free to correct me where I have done wrong and let's discuss this case together! Happy Simulating!

A 3 port 1/4 inch baffled manifold for normalized water flow out of 3 outputs from a single pressurized input

Analisa aliran udara dalam ruang isolasi di rumah sakit

This is a simulation for Lab 9 in fluid mechanics labeled, Computational Fluid Dynamics.

CFD analysis for a new surgical method for normal pressure hydrocephalus.

View conic section shape when rotate a fluid

this is an experiment on convergent and divergent tube

Goal of the project is to calculate pressure drop in a 3D Rectangular Channel with multiple 90 degree bends in which water is flowing with the Reynolds number of 51000. 
Further goal is  to optimize the pressure drop by adding vanes at the 90 degree channel bends.
The type of simulation is steady incompressible turbulent flow. 
5 times the hydraulic diameter extension is given as extension at the inlet in order to develop the flow and same extension is given after the real outlet in order to eliminate the impact of boundary condition on the domain of interest.

Understand fluid flow and heat transfer properties in a volume

To analys flow through pipe.
Compressible CFD simulation
Enough now! Let's get to project.

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

design a wind turbine that can work in tow direction .and make a simulation of the dynamic of fluid .

From Prandtl's 1933 paper on Bell lift distribution for minimizing the induced drag and recent works being published by NASA on PRANDTL D glider,  I decided to do a performance study and comparison of this type of lift distribution along with the conventional elliptic lift distribution,  that is to compare two wings with different lift distributions but with the same plan form area, taper ratio and aspect ratio

In this project we are analyzing the steady state heat transfer of a water cooled hot plate. The primary targets of the evaluation are to find the maximum temperature within the hot plate, the temperature change of the cooling fluid, and the pressure loss through the the water tube system. Solutions from the conjugate heat transfer CFD solution are compared to the theoretical solutions to determine the overall correlation of the values.

A chemically reacting fluid flows through a channel.Design considerations require that the flow area of the duct be abruptly
reduced to 1/10th of its size. To prevent destruction of the duct by the reacting fluid,no stagnant eddies at the contraction can be allowed.have some control over the duct length upstream of the contraction, and thus the velocity profile of the fluid approaching the contraction. To solve this problem, you must somehow
estimate the flow field near the contraction.