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Projects by Amey Pawade

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 of Supercycl Read more

Prandtl Meyer Shock Problem
Amey Pawade · 2019-03-01 07:59:53

Objectives: Simulate a supersonic flow through a duct having a sharp corner to observe the formation of Shock waves. Literature review on Shock waves. Literature review on Shock wave boundary conditions. Observe the effect of SGS parameter on shock wave location. Read more

Objectives of the Project: (1) Perform a transient simulation for the flow of air over a throttle body in Converge Studio and post-process the results in ParaView. (2) Show the plots for pressure, velocity, and mass flow rate. (3) The throttle valve should rotate by Read more

Objectives of the Project: (1) Calculation of Flow Variables. (2) Generation of blockMeshDict using the wedge boundary condition. Create the blockMeshDict file in MATLAB such that the mesh is automatically created for various wedge angle. (3) Simulating the pipe flow Read more

Objectives of the Project: (1) Perform a steady state simulation for the flow of air over a throttle body in Converge Studio and post-process the results in ParaView. (2) Show the plots for pressure, velocity, and mass flow rate.   Geometry: The throttle ins Read more

Objectives of the Project: (1) Calculation of Flow Variables. (2) Generation of blockMeshDict using the wedge boundary condition. Create the blockMeshDict file in MATLAB such that the mesh is automatically created for various wedge angle. (3) Simulating the pipe flow Read more

Project Objectives: (1) To simulate air flow through a Backward-facing step using CONVERGE Studio and Post-process using ParaView. (2) To conduct a grid independent test and study the Pressure and Velocity contour.   Geometry: length along x-axis = 0.27 m l Read more

Project Objectives: (1) To simulate the air flow through a channel using CONVERGE Studio and post-process using ParaView. (2) To conduct a grid independent test and study the Velocity and Pressure contour.   Mesh sizes: X-direction -  2e-4 m 1.5e-4 m Read more

Objectives of the Project: (1) Create the geometry using BlockMesh in OpenFOAM. (2) Simulate the flow using the icoFoam solver. (3) Compare the velocity magnitude profile for different values of mesh grading factor at a distance of 0.085m from the inlet. Theory: Fo Read more

Objectives of the Project: (1) Solve the Conservative and Non-conservative form of governing equation of Quasi 1-D Supersonic nozzle flow using the Maccormack method. (2) Compare the results of the Conservative and Non-conservative form. (3) Perform Grid depende Read more


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