Modeling and Simulation of Airflow around an Ahmed Body for a 35-degree slat using converge studio

                        FLOW OVER A NACA 2412 AIRFOIL USING CONVERGE STUDIO.   OBJECTIVE: Simulate flow over a 4 digit airfoil i.e NACA 2412 Airfoil. I have to calculate the following, Drag co-efficient…

BlockMesh Drill down challenge: Specification The number of cells along the direction of flow = 200 The number of cells along the y-direction for each block = 10 Inlet Velocity is 1 m/sec.  Boundary condition specification Follow the specifications that are provided in the following figure. Desired output Run the…

Simulation of a 1D QUASI Super-sonic nozzle flow simulation using Macormack Method Introduction Your objective in this project is to write code solve the 1D supersonic nozzle flow equations using the Macormack Method. You will be implementing both the conservative and non-conservative forms of the governing equations You…

Taylor table method and Matlab code   Derive the following 4th order approximations of the second-order derivative 1. Central difference 2. Skewed right-sided difference 3. Skewed left-sided difference Once you have done this, write a program in Matlab to evaluate the second-order derivative of the analytical function…

CHANNEL FLOW SIMULATION USING CONVERGE CFD The main objective of the project is to simulate the simple 2D channel flow in Converge CFD software. The simulation is done for three different base mesh and compared with respect to plots of velocity, pressure, total cell count and mass flow rate in all the meshes and also show…

  Modeling and Simulation of Airflow around an Ahmed Body for a 35-degree slat using converge studio   Objective: Create the CAD model using CATIA as per dimensions (35-degree slant) Setup a Coarse CFD simulation  Setup the virtual wind tunnel as shown in the video Apply the right boundary conditions and…

Geometry cleanup WindTunnel set up and CFD Simulation of a Formula FSAE car for two different racing conditions ( Lot of turns and straight) using converge studio and paraview   The main objective of this project is to perform geometry clean up,  boundary flagging, virtual wind tunnel, pre-processing, CFD simulation…

Shock tube simulation project OBJECTIVE: Setup a transient shock tube simulation Plot the pressure and temperature history in the entire domain - Explain the result Plot the cell count as a function of time - Explain the result SHOCK TUBE DESCRIPTION: The shock tube is divided into two regions namely low and high-pressure…

Conjugate Heat Transfer Simulation in Converge Studio     Objectives: Simulate flow of air through a solid pipe and study the heat transfer from the walls of the pipe to the fluid flowing inside the pipe. Run a grid dependence test to see the effect of changing grid size on the heat transfer. Study the effect…

Prandtl Meyer Shock Problem Objectives: Simulate a supersonic flow through a duct having a sharp corner to observe the formation of Shock waves. Literature review on Shock waves and explain physics behind the shock waves. Literature review on Shock wave boundary conditions. Observe the effect of SGS parameter on shock…

Project Transient simulation of flow over a throttle body The throttle body moves as follows: From 0 to 2 ms the valve should rotate by 25 degrees. From 2 to 4ms it should stay at 25 degrees. After which by 8ms the valve should get back to its original position Elbow Channel Case Description: Elbow Channel consists of…

Project Steady-state simulation of flow over a throttle body:   Elbow Channel Case Description: Elbow Channel consists of a throttle valve which lies between the inlet and outlet. The geometry bounding box should be enabled to find the value of dimensions. The throttle valve remains stationary and we are going to…