ANSA - CFD meshing on Turbocharger

AIM:- A. To Perform a Heat Transfer Analysis on A battery set by Inlet Velocities and Gap Between the Batteries. B. The Explain the Relevant  Results Generated by the Analysis.   Given:- A. The Battery Set Geometry: -   The Following are the Parameters for the Battery Set: -      i. The…

AIM: - A. To Perform Simulation on the Gate Valve by Setting the Opening from 10% to 80% B. To Calculate the Mass Flow rate and the Flow Factor for each Case   Given: - A. The Given CAD Models of Gate Valves: -                              …

AIM: - A. To Perform the Analysis of the Given Cyclone separator for different particle sizes and different inlet speeds. B. To Explain the relevant theories and to explain the generated results   Given and Assumed: - A. The Geometry of the Given CAD Model: -   B. Material and their Properties:…

Problem Statement: - Perform a Steady State CHT analysis on the Given Graphic Card Model for 3 inlet Velocities 1 m/sec, 3 m/sec, and 5 m/sec for Course and Fine Mesh. Create an appropriate Mesh, define appropriate Materials for each Component and Perform a mesh-independent Study.   Expected Results: - 1. Explain…

AIM: - A. To Perform a Rayleigh Taylor Instability Simulation using Air and Water Combination and User-defines Fluid and Water Combination. B. Simulate Rayleigh Taylor Instability for Course and Fine Mesh and Explain the difference of results between both for Air and Water Combination. C. Simulate Rayleigh…

Problem Statement: - For the Given Ahmed's Body Perform a CFD analysis for an inlet Velocity of 25 m/sec and Generate the Appropriate Contours and Plot. Also, Calculate the Values of Drag experienced by Ahmed's Body and Perform a Grid Independence Study Expected Results: - 1. Create a Computational domain for this analysis.…

Problem Statement: - For a 2m diameter Cylinder. Perform a CFD Simulation to Analyse Flow over the Cylinder for Reynolds Numbers 10, 100, 1000, 10000, 100000 Expected Results: - 1. Create the required 2D geometry and desired Computational Domain. 2. CFD Simulation of Flow over a Cylinder with required Physics settings…

Problem Statement: - Simulate A Quasi 1D Subsonic-Supersonic Nozzle using Conservative and Non-Conservative Forms of Governing Equations using MacCormack Technique. Desired Objectives: - 1. Derive These governing Equations and Non-Dimensionalise them. 2. Use appropriate Boundary Conditions 3. Compare The Variables in Conservative…

AIM: - A. To Perform a CHT Analysis on the given Exhaust Port with proper y+ values and explain the proper theory. B. To Calculate the Heat Transfer Coefficient on the internal Surface and to verify its accuracy.   Given: - A. The Given CAD Model of The Exhaust Port: -   B. Conditions at Inlet,…

Problem Statement: - For the Given Mixing Tee Geometries where one is Long and the other is Short. Perform a CFD analysis using Ansys Software when for the given geometry Hot Fluid is entering the Tee along the X direction at `36^@C` and Cold Fluid is entering the Tee along the Y direction at `19^@C`. The Following…

Problem Statement: - For the given models, check and solve all geometrical errors and Assign appropriate PIDs. Perform meshing using Surface Wrap with the given Target length of 3mm   Solution: - AIM: - A. To Perform Geometric Cleanup of Engine, Gearbox, and Transmission. B. To Perform Surface Wrapping of…

Problem Statement: - For the given model, check and solve all geometrical errors and Assign appropriate PIDs. Perform meshing with the given Target length and element Quality criteria. Create A wind Tunnel for analysis and Assign appropriate PIDs. The target lengths for all PIDs are given below: - 1. Body - 4mm 2. Tires…

Problem Statement: - For the given model, check and solve all geometrical errors and Assign appropriate PIDs. Perform meshing with the given Target length and element Quality criteria. Create A wind Tunnel for analysis and Assign appropriate PIDs. The target lengths for all PIDs are given below: - 1. Body - 3mm 2. Lights…

Problem Statement: - For the given model, check for the geometrical errors to make appropriate volumes. Create and assign PIDs, Perform surface mesh with the given target lengths as per PIDs. Blade stage-1 = 1 mm Blade stage-2 = 1 mm Impeller = 2 mm Shaft rotor = 1 mm Turbo casing = 5 mm Compressor casing = 5 mm Inlet…

Problem Statement: -For the given model, check for the geometrical errors and perform Topology cleanup accordingly. Set three different target lengths as three different cases and mesh the model. Target length = 1mm, 3 mm and 5 mm (i.e. 3 cases) Element type = Tria Apply any one target length from the above at a time for…

Problem Statement: - For A 2D surface maintained at a certain temperature at its edges. Solve using Iteration Methods(Jacobi, Gauss-Seidel, and S.O.R. using Gauss-Seidel) for Temperature distribution due to Heat Conduction that can be observed for the following States: - 1. Transient State until Steady State is Achieved…

Problem Statement: - For the Function `f(x) = e^x*cos(x)` derive the 4th Order Accurate Approximation of 2nd Order Derivative for the given function using Taylor Table Method for the following difference Methods: - 1. Central Difference 2. Skewed right-sided difference 3. Skewed left-sided difference Write A MATLAB…