https://projects.skill-lync.com/projects/Pipe-Flow-Simulation-using-Solidworks-32626

This project is focused on simulating the NACA airfoil for the different angle of attacks mainly 0°, 2°, 4°, 6°, 8° & 10°. The lift & drag forces are compared for the same.   Using the sample data for the airfoil points, Airfoil was created in SolidWorks and extruded for the 3D…

Inputs considered for the baseline simulation: cylinder diameter (D) = 0.02m inlet velocity (u) = 10 m/s Using the formula, Re = (density * inlet velocity * diameter) / dynamic viscosity where ; density of air = 1.225 kg/m³ dynamic viscosity = 1.81E-5   From the formula, Reynolds Number for baseline simulation…

I have used following data for my simulation: Length= 1m Diameter= 0.06m lines probes were set at 95%, 90% and 85% (i.e. 950mm, 900mm & 850mm) of the length Shell was created Flow Simulation Water was used as the medium for simulation. The simulation was conducted for 3 different values of Reynolds number: 1.…

When the cyclist rides the bike, it encounters drag force due to the wind and velocity. `F_d = 1/2 rho A v^2 C_d` where  `F_d`is the drag force in `kg m/sec^2` `rho` is the air density in `(kg)/m^3` `A`is the frontal area in `m^2` `v` is the velocity in `m^2/sec^2` `C_d` is the coeffecient of drag…

Case setup: 1. Valve lift = 0.002 m 2. Boundary conditions:     Inlet pressure= Total pressure 101325 Pa     Outlet pressure= Static pressure 95000 Pa 3. Goals:      SG Mass Flow Rate1 for measuring the mass flow rate coming out of the outlet   A. Grid Dependence test: Valve…

CAD model has created keeping in mind the data provided in the video. For the Flow Simulation following parameters and conditions are used- 1. Rotating Region: Angular velocity of rotating blades is selected as 1000 rad/sec. 2. Boundary Conditions:     Inlet pressure = 101325 Pa     Outlet velocity…