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Taylor table method and Matlab code

From the Taylor Table method, the fourth-order approximation of second-order derivative has been derived.  Central Difference: `(d^2 f)/(dx^2 )=(-0.0833*f(i-2)+1.3333*f(i-1)-2.500*f(i)+1.3333*f(i+1)-0.0833*f(i+2))/dx^2` Skewed Right Side Difference: `(d^2 f)/(dx^2 )=(0.6753*f(i)-0.5977*f(i+1)-1.2586*f(i+2)+1.6092*f(i+3)-0.4282*f(i+4))/dx^2`…

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    Read more Projects by Argha Saha (6)

    Symmetry vs Wedge vs HP equation

    Objective:

    All the inputs have been discussed in the exercise of the week - 11. For 10 degree angle in symmetry boundary condition, all the samples have been given here. For the rest, these will be almost same.  MATLAB Programme to generate block mesh file for 10 degree: clear all close all clc %% Inputs L = 1.5; theta = 10;…

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    24 Nov 2019 02:00 PM IST

    • CFD
    • MATLAB
    Read more

    Simulation of Flow through a pipe in OpenFoam

    Objective:

    Density of water = 998 kg/m3 Dynamic viscosity of water = 8.90 *10-4 Pa. s Reynolds no = 2100 Let the Diameter = 0.01 m Inlet velocity = 0.1874 m/s Entry length for a laminar pipe is = L = 0.05*Re*D = 1.05 m Therefore for the simulation, a length of 1.5 m has been taken which is greater than the entry length. According…

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    20 Nov 2019 11:15 PM IST

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    BlockMesh Drill down challenge

    Objective:

    BlockMesh Coding: /*--------------------------------*- C++ -*----------------------------------*\\ ========= | \\\\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\\\ / O peration | Website: https://openfoam.org \\\\ / A nd | Version: 7 \\\\/ M anipulation | \\*---------------------------------------------------------------------------*/…

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    19 Nov 2019 08:41 AM IST

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    Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method

    Objective:

    Non-Conservative Function: function [rho,v,T,a,x,mach,q,mass_flow,rho_throat,Temp_throat, mach_throat, Pr_throat, m_throat,k] = non_conservative(L,n,nt) x = linspace (0,L,n); dx = x(2)-x(1); gamma = 1.4; %% Initial profiles rho = 1-0.3146*x; %rho =density T = 1- 0.2314*x; %T = temperature v = (0.1 +1.09*x).*T.^0.5; %v…

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    19 Nov 2019 12:44 AM IST

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      Steady and unsteady 2D heat conduction problem

      Objective:

      STEADY STATE: Matlab Code: clear all close all clc %% Initial and Boundary conditions L = 1; nx = 81; ny = nx; dx = L/(nx-1); dy = dx; %w = 1.1; T = 298* ones(nx,ny); T(1,:) = 900; % Bottom (1st row is being counted from bottom) T(:,1) = 400; % Left T(:,end) = 800; % Right T(end,:) = 600; % Top % Corner points T (1,1)…

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      17 Nov 2019 02:38 AM IST

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        Taylor table method and Matlab code

        Objective:

        From the Taylor Table method, the fourth-order approximation of second-order derivative has been derived.  Central Difference: `(d^2 f)/(dx^2 )=(-0.0833*f(i-2)+1.3333*f(i-1)-2.500*f(i)+1.3333*f(i+1)-0.0833*f(i+2))/dx^2` Skewed Right Side Difference: `(d^2 f)/(dx^2 )=(0.6753*f(i)-0.5977*f(i+1)-1.2586*f(i+2)+1.6092*f(i+3)-0.4282*f(i+4))/dx^2`…

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        14 Nov 2019 06:40 AM IST

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          Showing 1 of 6 projects