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Devang Patel

Skills Acquired at Skill-Lync :

  • CFD
  • NUMERICAL-ANALYSIS
  • MATLAB
  • OPENFOAM
  • AERODYNAMICS
  • CONVERGE-CFD

22 Projects

Prandtl Meyer Shock in Converge Studio

Objective:

AbstractThe purpose of this project is to simulate the Prandtl-Meyer Shock wave using Converge Studio and study how adaptive mesh refinement (AMR) affects the results. IntroductionShock waves, also known as compression waves, is a type of developing disturbance that moves faster than the local speed of sound in the medium.…

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26 Aug 2019 08:11 AM IST

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    Understanding Linear System and effect of Spectral Radius

    Objective:

    Linear System Linear system of equations and be written in matrix form as,           `Ax = b` where:           We can decompose the coefficient matrix into Diagonal component, `D`, and strictly Lower, `L`, and strickly upper Upper,…

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    09 Nov 2019 12:22 PM IST

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      Steady vs Transient Flow over Cylinder in ANSYS Fluent

      Objective:

           

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      27 Jun 2020 09:34 PM IST

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        Shock Tube Simulation in Converge Studio

        Objective:

        AbstractThe purpose of this project is to simulate a Shock Yube using Converge Studio and understand the process behind setting up the simulation.  IntroductionLet us first define the basic concept of Shock Tubes. A shock tube is a simple duct closed at both ends, which is divided into two region- driver and driven…

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        08 Aug 2019 05:12 PM IST

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          OpenFOAM BlockMesh Challenge

          Objective:

          ObjectiveTo simulate flow over the backward-facing step in OpenFOAM and study the effect of mesh grading factor on the simulation result. Requirements Number of cells along the x-direction (longer dimension) = 200 Number of cells along with the y-direction = 10 Use a graded mesh. Compare the results of mesh grading factors…

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          15 Feb 2020 01:09 PM IST

          • CFD
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          Steady State and Transient State 2D Heat Conduction

          Objective:

          3D Transient Heat Conduction can be written as following when there is no source term.            `(partialT)/(partialt) + alpha((partial^2T)/(partialx^2) + (partial^2T)/(partialy^2) + (partial^2T)/(partialz^2)) = 0` For our project, we will be looking at a 2D Heat…

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          31 Oct 2019 11:09 AM IST

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            Channel flow simulation using CONVERGE CFD

            Objective:

            AbstractIn this project, simple channel flow was simulated using CONVERGE Studio and compare the results of three different mesh grid size. Then it was post-processed in ParaView to understand the results visually. CYGWIN was used to run the commands for simulation and convering the files for the post-processer.  …

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            06 Jul 2019 11:31 AM IST

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              Conjugate Heat Transfer Simulation in Converge Studio

              Objective:

              AbstractThe purpose of this project is to simulate Conjugate Heat Transfer in Converge Studio and study how super-cycle affects the computational time. MethodThe circular pipe was created in Converge Studio with an inner diameter of 0.015 m (15mm) with the wall thickness of 0.005m (5mm), as shown in Figure 1. Once the…

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              25 Jul 2019 08:34 PM IST

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                Quasi-One Dimensional Supersonic Nozzle Solution using Macormack Method

                Objective:

                ObjectiveThe objective for this project is to simulate 1D Super-sonic nozzle flow using Macormack Method   MacCormack MethodIn Computational Fluid Dynamics (CFD), MacCormack method is discretization scheme for the numerical solution of partial differential equations (PDE). The MacCormack method is a simpler variation…

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                02 Feb 2020 03:26 PM IST

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                Flow over an NACA 2412 Airfoil

                Objective:

                AbstractThe purpose of this project is to simulation flow over NACA 2412 Airfoil in Converge Studio and examine how the angle of attack affects drag and lift on the airfoil. IntroductionAirfoil is a cross-sectional shape of a wing which produces aerodynamic force when in motion.  The aerodynamic force is a resultant…

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                26 Aug 2019 09:12 PM IST

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                  Effect of Length and Momentum Ratio on Mixing Efficiency using ANSYS FLUENT

                  Objective:

                  AbstractThe purpose of this project is to simulate the flow inside a T-junction pipe and compare the effect of different length geometry and speeds of two fluids at different temperatures on the mixing. IntroductionA T-junction pipe, or mixing tee, as the name states is a t-shape pipe where two-fluid or air comes from…

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                  09 Apr 2020 12:17 PM IST

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                    Project Transient simulation of flow over a throttle body

                    Objective:

                    AbstractIn this project, a flow inside a curve pipe with rotating throttle inside was simulated using CONVERGE Studio and view the results of the simulation. After the simulation, the project was post-processed in ParaView to understand the results visually. Visualization was taken from ParaView and Plots were made in…

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                    06 Jul 2019 05:44 PM IST

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                      Fourth Order Approximation of the Second Derivative

                      Objective:

                            Results and Discussion   FIGURE 1: Error versus grid size for fourth-order approximation for second derivative using Central, Right Skewed, Left Skewed, Forward Difference, and Back Difference Scheme. In the above plot, Figure 1, we can see that the lower value of delta x, the error decreases.…

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                      14 Oct 2019 05:59 PM IST

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                        Flow over a backward facing step

                        Objective:

                        AbstractIn this project, flow over a backward step was simulated in CONVERGE Studio, and compared the results of three different mesh grid size. The project was then post-processed in ParaView to understand the result visually. CYGWIN was use to run the simulation commands and convert files for the post-processing.  …

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                        27 Jun 2019 01:20 PM IST

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                        Analysis of Aerodynamic Forces over Forumla SAE Car

                        Objective:

                        Introduction:Formula SAE, commonly known as FSAE, is a student design competition organized by Society of Automotive Engineers (SAE). In the growing technology and engineering process, Computational Fluid Dynamics (CFD) has played a huge role in the design of such aerodynamic cars. CFD analysis on an FSAE car can give…

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                        14 Sep 2019 04:36 PM IST

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                        Modeling and Simulation of flow around an Ahmed Body

                        Objective:

                        IntroductionThe Ahmed body is a generic car body. The airflow around the Ahmed body captures the essential flow features around an automobile and was first defined and characterized in experimental work of S.R. Ahmed in 1984. In this project, external flow simulation over an Ahmed Body was performed and results were compared…

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                        14 Sep 2019 09:57 PM IST

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                          Project Steady state simulation of flow over a throttle body

                          Objective:

                          AbstractIn this project, a flow inside a curve pipe with a throttle inside was simulated using CONVERGE Studio and view the results of the simulation. After the simulation, the project was post-processed in ParaView to understand the results visually. Visualization was taken from ParaView and Plots were made in Converge…

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                          06 Jul 2019 12:31 PM IST

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                            Channel flow simulation using CONVERGE CFD

                            Objective:

                            AbstractIn this project, simple channel flow was simulated using CONVERGE Studio and compare the results of three different mesh grid size. Then it was post-processed in ParaView to understand the results visually. CYGWIN was used to run the commands for simulation and convering the files for the post-processer.  …

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                            25 Jun 2019 03:46 PM IST

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                              Literature review RANS derivation and analysis

                              Objective:

                              Reyonlds-Averaged Navier-Strokes (RANS) equations are time-averaged equations of motion used to describe turbulent fluid flow.  To derive the equation, Reynolds decomposition must be used. Reynolds decomposition separates the flow variable into the mean and the fluctuating component as shown below. `u = obrace(baru)^(\"mean\")…

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                              09 Nov 2019 03:39 PM IST

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                                Ahmed Body Challenge

                                Objective:

                                   

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                                27 Jun 2020 09:43 PM IST

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                                  Exhaust Port Challenge

                                  Objective:

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                                  13 Aug 2020 07:04 PM IST

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                                    Rayleigh Taylor Instability Challenge

                                    Objective:

                                      Animation Files Baseline Simulation Animation Case 1 Simulation Animation Case 2 Simulation Animation Case 3 Simulation Animation

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                                    30 Dec 2020 02:31 AM IST

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                                      2 Course Certificates

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                                      Advanced Aerodynamic Simulations using CONVERGE

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                                      Introduction to CFD using MATLAB and OpenFOAM

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