matlab program is written to simulate the 1-D super sonic nozzle flow using Macormack Method , A comparison is made between conservative and non conservative form of governing equation to check which one is faster and how the parameters changes along the length of the nozzle in both the forms, a separate program is written…
Dinesh Kumar
updated on 14 Jun 2019
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Read more Projects by Dinesh Kumar (34)
Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method
matlab program is written to simulate the 1-D super sonic nozzle flow using Macormack Method , A comparison is made between conservative and non conservative form of governing equation to check which one is faster and how the parameters changes along the length of the nozzle in both the forms, a separate program is written…
14 Jun 2019 06:17 AM IST
Steady state vs unsteady analysis
1. The fastest simulation in steady state, transient implicit and transient explicit is the successive over-relaxation method, the number of iterations in which solution converges in case of steady state is around 30 while in the transient explicit mode the number of iteration in which solution converges is 197 and in…
14 Jun 2019 06:15 AM IST
Solving the steady and unsteady 2D heat conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Jun 2019 06:15 AM IST
Linear Convection
The figure shown below illustrates the variation of velocity after 0.4 seconds with the grid size, as the grid size increases from 21 to 81 the velocity profile start taking its original form but at a grid size of 161, the grid becomes finer some instabilities start forming and systems become unstable clear all close…
14 Jun 2019 06:14 AM IST
Taylor table method and Matlab code
the figure shown below shows the curve for different skewed technique, from the figure it is clearly visible that the central skewed scheme gives the least error of all three schemes and left skewed scheme to give the low magnitude of error to compare to right skewed error.all the schemes follows nearly same trend. I think…
14 Jun 2019 06:11 AM IST
Discretization basics
google link for Matlab program of discretization basics https://drive.google.com/open?id=1vMOEB6ZRkbz1Xfz5-rGJJ1J-ZP0_pV-8 the above figure shows the comparison of the first order, second order and fourth order approximation of analytical vs exact derivative. from the figure, it can be concluded that…
14 Jun 2019 06:09 AM IST
Boundary and initial conditions
boundary conditions are essential to obtain a solution of a boundary value problem, Boundary conditions are defined at the boundary of an independent variable in an equation whereas in initial value condition has all of the condition defined at the same value of the independent variable in an equation. for example, boundary…
14 Jun 2019 06:04 AM IST
Stability analysis in the unsteady problem
1. Explicit Method : In case of a transient explicit method, stability largely depends on CFL number CFL number for 2-dimensional heat conduction problem is given as: k= alpha* (dT/dx² + dT/dy²) ≤ 0.5 in this case dx = dy hence CFL ≤ 0.25, where alpha is thermal diffusivity…
14 Jun 2019 06:04 AM IST
FVM Literature Review
Interpolation Schemes: 1. Upwind Interpolation: It is used for calculating approximate value of wariable at the east face of control volume, it is first order accurate and is numerically diffusive with coefficient of numerical diffusion. It is equivalent to using a backward or forward finite difference approximation. The…
19 Dec 2018 11:37 AM IST
Literature review RANS derivation and analysis
link for Derivation of Reynolds average naviers strokes equation is given below. https://drive.google.com/open?id=1lkwLuP7szfQ_zHaSwchncw8mGyco2sR3 https://drive.google.com/open?id=1Atmk8O_TLE15zXa2Zk_q3QvM8SpnCRfa
17 Dec 2018 10:17 AM IST
Surface preparation and Boundary Flagging
Objective: The objective was to import and clean up the port fuel engine geometry from all types of error. and after that boundary flagging is done. First the geomerty is imported in Converge Studio for analysis and to clean up the geometry errors. the Following Figure shows the geometry imported in Converge. after…
17 Dec 2018 10:01 AM IST
Shock tube simulation project
A shock Tube simulation is setup in Converge Studio for analysis. During the case setup the whole shock tube is divided into two regions i.e. high pressrue region and low pressure region.In the high pressure region Nitrogen gas is filled where as in low pressure region oxygen gas is filled. Initially the high pressure…
17 Dec 2018 10:01 AM IST
Prandtl Meyer Shock problem
Boundary Conditions: Depends on the type of flow, boundary conditions varied like for solving steady state problem appropriate boundary condition are used. and for solving transient flow equations appropriate initial conditions are used. Types of Boundary Conditions. 1. Drichlet Boundary Condition. In case of drichlet…
17 Dec 2018 10:00 AM IST
Project Transient simulation of flow over a throttle body
Objective: To study the transient flow over a throttle which is placed inside a pipe. the throttle initially remains in horizontal direction and then moves at an angle of 25 degree stay their for 4 ms and then comes back to initial position. The figure shown below shows the throttle position at initial time. after this…
17 Dec 2018 09:59 AM IST
Project Steady state simulation of flow over a throttle body
Objective: To study the steady state simulation over a throttle body. in this problem we will study how the flow behaves over the throttle. Th figure shown below shows the throttle valve inside the pipe. A valve is placed inside the pipe which restricts some area of flow. the flow takes place due to pressure difference.…
02 Dec 2018 12:25 PM IST
Symmetry vs Wedge vs HP equation
Objective: To study the effect of changing of boundary condition from wedge to symmetry. and check whether there is any deviation of parameters like pressure or velocity from theoretical equation. Theory: wedge boundary condition is used if the wedge angle is less than 5. while for wedge angle greater than 5 symmetry boundary…
02 Dec 2018 06:13 AM IST
BlockMesh Drill down challenge
Objective: the objective of this study is to make a backward facing step block by editing blockMeshDict file and simulate it in openfoam and post process the result like velocity profile near the step zone and to check the effect of grading scheme. on velocity profile. first the backward step facing block is divided…
30 Nov 2018 03:27 AM IST
Simulation of Flow through a pipe in OpenFoam
OBJECTIVE: To write a program in Matlab which will generate BlockMeshDict file automaticlly of given grading schemes and wedge conditions. and to study the flow through a pipe in OpenFoam and validate the results with theoretical equations which is Hagen poiseuille\'s equation. GIVEN: Reynolds Number - 2100 Radius of pipe…
29 Nov 2018 10:59 PM IST
a new title
#commentUse insert code to paste your codes The figure shown below illustrates the effect of the number of moles on the stoichiometric coefficient in the case of alkyne, alkene, and alkanes. the trend shows that the variation is linear in all three caseshttps://drive.google.com/open?id=1q3t_6R2j7lzh3i3yZVL8vRzOg3d9Cjm4
26 Nov 2018 07:08 AM IST
a new title
boundary conditions are essential to obtain a solution of a boundary value problem, Boundary conditions are defined at the boundary of an independent variable in an equation whereas in initial value condition has all of the condition defined at the same value of the independent variable in an equation.for example, boundary…
26 Nov 2018 07:07 AM IST
1-D supersonic nozzle flow simulation using macormack method
matlab program is written to simulate the 1-D super sonic nozzle flow using Macormack Method , A comparison is made between conservative and non conservative form of governing equation to check which one is faster and how the parameters changes along the length of the nozzle in both the forms, a separate program is written…
22 Oct 2018 01:35 PM IST
stability analysis in Unsteady state
1. Explicit Method : In case of a transient explicit method, stability largely depends on CFL number CFL number for 2-dimensional heat conduction problem is given as: k= alpha* (dT/dx² + dT/dy²) ≤ 0.5 in this case dx = dy hence CFL ≤ 0.25, where alpha is thermal diffusivity…
15 Sep 2018 02:08 AM IST
Steady state vs Unsteady analysis
1. The fastest simulation in steady state, transient implicit and transient explicit is the successive over-relaxation method, the number of iterations in which solution converges in case of steady state is around 30 while in the transient explicit mode the number of iteration in which solution converges is 197 and in…
15 Sep 2018 12:41 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
2D Heat Conduction problem
The temperature distribution curve for 2D steady state conduction equation is shown below,from the figures it is clearly visible that the number of iterations in which solution converges starts decreasing from Jacobi to SOR, in case of Jacobi the number of iterations is 216 while in case of gauss seidel it…
14 Sep 2018 04:04 AM IST
Variation of Stoichiometric co-efficient on number of moles of carbon
The figure shown below illustrates the effect of the number of moles on the stoichiometric coefficient in the case of alkyne, alkene, and alkanes. the trend shows that the variation is linear in all three cases https://drive.google.com/open?id=1q3t_6R2j7lzh3i3yZVL8vRzOg3d9Cjm4
13 Sep 2018 01:40 PM IST
Linear Convection Grid Dependence Problem
The figure shown below illustrates the variation of velocity after 0.4 seconds with the grid size, as the grid size increases from 21 to 81 the velocity profile start taking its original form but at a grid size of 161, the grid becomes finer some instabilities start forming and systems become unstablehttps://drive.google.com/open?id=175t4A3jXD5IysU-t_G5ntWuRhb7MokAo
13 Sep 2018 01:25 PM IST
table taylor method
the figure shown below shows the curve for different skewed technique, from the figure it is clearly visible that the central skewed scheme gives the least error of all three schemes and left skewed scheme to give the low magnitude of error to compare to right skewed error.all the schemes follows nearly same trend. I think…
13 Sep 2018 06:35 AM IST
Week 3 - Discretization basics
google link for Matlab program of discretization basics https://drive.google.com/open?id=1vMOEB6ZRkbz1Xfz5-rGJJ1J-ZP0_pV-8 the above figure shows the comparison of the first order, second order and fourth order approximation of analytical vs exact derivative. from the figure, it can be concluded that…
08 Sep 2018 12:55 PM IST
Boundary and initial conditions
boundary conditions are essential to obtain a solution of a boundary value problem, Boundary conditions are defined at the boundary of an independent variable in an equation whereas in initial value condition has all of the condition defined at the same value of the independent variable in an equation. for example, boundary…
06 Jul 2018 04:57 AM IST