AIM:- To perform transient and steady-state analysis of temperature evolution for a 2D domain with the given boundary conditions: Top Boundary = 600 K Bottom Boundary = 900 K Left Boundary = 400 K Right Boundary = 800 K And to compare the explicit and implicit methods of Jacobi, Gauss-Seidel, and Successive Over-Relaxation…
Rahul Bhaval Das
updated on 15 Feb 2021
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Read more Projects by Rahul Bhaval Das (10)
Week 12 - Validation studies of Symmetry BC vs Wedge BC in OpenFOAM vs Analytical H.P equation
AIM:- To compare between the numerical results obtained for incompressible, laminar pipe flow using OpenFOAM with the wedge and symmetry boundary conditions and also to compare the results with the analytical results based on the Hagen-Poiseulle equation. The numerical simulation is done for portions/wedges of the pipe…
15 Apr 2021 10:59 AM IST
Week 11 - Simulation of Flow through a pipe in OpenFoam
AIM:- To simulate laminar-incompressible flow through a pipe using OpenFOAM using axisymmetric wedge boundary condition and MATLAB and validate with results obtained from Hagen-Poiseulle equation for fully developed flow. MATLAB is used to automate the generation of the blockMeshDict file taking inputs like pipe diameter,…
20 Mar 2021 07:47 PM IST
FVM Literature Review
Finite Volume Method (FVM) is a discretization method used to convert integral forms of governing equations into algebraic equations. This method is inherently conservative due to the use of the integral forms of the equations. The properties of the discretization method required for the numerical results…
15 Feb 2021 05:20 AM IST
Simulation of a backward facing step in OpenFOAM
AIM:- To use OpenFoam to simulate incompressible-viscous-laminar flow through a backward-facing step with the mesh being created using blockMesh. The effect of the grading factor is also analysed. THEORY:- OpenFoam is an open-source CFD software that uses C++ code and blockMesh is a mesh generator in OpenFoam. The…
15 Feb 2021 05:19 AM IST
Simulation of a 1D Supersonic nozzle flow simulation using MacCormack Method
AIM:- To use the MacCormack method to solve the 1-dimensional convergent-divergent nozzle flow problem with the initial conditions provided for both conservative and non-conservative forms of the governing equations. THEORY:- A convergent-divergent nozzle is a nozzle that has a decreasing (convergent) area…
15 Feb 2021 05:19 AM IST
Solving the steady and unsteady 2D heat conduction problem
AIM:- To perform transient and steady-state analysis of temperature evolution for a 2D domain with the given boundary conditions: Top Boundary = 600 K Bottom Boundary = 900 K Left Boundary = 400 K Right Boundary = 800 K And to compare the explicit and implicit methods of Jacobi, Gauss-Seidel, and Successive Over-Relaxation…
15 Feb 2021 05:18 AM IST
Taylor table method and MATLAB code
AIM:- To calculate the second-order derivative of the following function:- `f(x) = exp(x)*cos(x)` using central difference, skewed forward difference, and skewed backward difference schemes of fourth-order accuracy. THEORY:- The formula for the discretized derivative in each of the schemes is obtained using the Taylor…
15 Feb 2021 05:18 AM IST
Parsing NASA thermodynamic data using MATLAB
AIM:- To develop a program that will parse the NASA Thermodynamic data file and calculate the specific heat, entropy, and enthalpy values for each of the species within their respective local temperature ranges and store their plots with respect to temperature in separate folders. The molecular weight of each of…
15 Feb 2021 05:17 AM IST
Genetic Algorithm
AIM:- To identify the maximum value of the stalagmite function using the inbuilt MATLAB genetic algorithm function while also studying the behavior of the genetic algorithm during 3 different cases: Unbounded search-space. Bounded search-space. Increased generated population space. INTRODUCTION:- Stalagmite function…
15 Feb 2021 05:17 AM IST
Solving second order ODEs
AIM To model and create the animation of a simple pendulum-bob system with damping whose motion is described by the 2nd order ODE - `(d^2theta)/dt^2+b/m*(d theta)/dt+g/l*sintheta=0` where theta - angular displacement of the bob from the mean position d theta/dt - angular velocity of the bob t - time m…
15 Feb 2021 05:16 AM IST