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Aditya Dube

Curious of the dynamics between machine and man with an understanding of Aerodynamics and CFD.

Skills Acquired at Skill-Lync :

  • CFD
  • AERODYNAMICS
  • CONVERGE-CFD

Introduction

I am a Mechanical Engineering Student from Lokmanya Tilak College Of Engineering, Navi Mumbai. My key interest is in CFD and Aerodynamics. Love studying about new advancements in the Automotive & Aviation industry and in the process learn as much as I can. I was also part of the SAE BAJA team of my college. Also competed in many SAE BAJA events nationally and internationally. This page is meant to serve as documentation for all the projects I have done. Please have a look and if there's anything to ask, please contact me at adityadube005@gmail.com.

17 Projects

Conjugate Heat Transfer Simulation

Objective:

Objective: The objective of this project is to set up conjugate heat transfer flow simulation through different conditions as mentioned below using Converge CFD.  Input for simulation= Reynolds number is 7000. Grid dependence Test Effect of super cycling w.r.t to three stage intervals- 0.01, 0.02, 0.03 seconds. Introduction:…

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09 May 2020 05:32 AM IST

  • CFD
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Aerodynamic Simulation over FSAE car

Objective:

Objective: To calculate the total downforce for the individual components of cars and any improvement in the components.  Aerodynamics Components: A Formula One race car is defined as much by its aerodynamics as it is by its powerful engine. That's because any vehicle travelling at high speed must be able to do two…

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20 Apr 2020 01:54 PM IST

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    Transient Simulation of Flow of Air over Throttle Body

    Objective:

    Objective: The objective of this project is to simulate the steady-state airflow through a throttle body by using Converge CFD.  Introduction: A throttle is a mechanism by which fluid flow is managed by constriction or obstruction. The term throttle has come to refer, informally, to any…

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    13 Jul 2019 08:21 AM IST

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    Understanding Linear systems

    Objective:

    In this project, we will write computer programs to manually determine the Eigen Value and Spectral Radius of the given system of equations. Also, solve them using iterative techniques like JACOBI, GUASS SEIDEL, SOR. The linear systems given are: `A=((5 ,1, 2) , (-3, 9, 4), (1 ,2, -7))` `X=((x1),(x2),(x3))` Computing…

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    09 May 2020 05:30 AM IST

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    Shock Tube transient Simulation

    Objective:

    Objective: The objective of this project is to perform a shock tube simulation using Converge CFD.  Introduction: The shock tube is an instrument used to replicate and direct blast waves at a sensor or a model in order to simulate actual explosions and their effects, usually on a smaller scale. Shock tubes…

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    04 May 2020 02:44 AM IST

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    Effect of time step on linear convection

    Objective:

    LINEAR CONVECTION: This equation is the most accessible in CFD; from the Navier Stokes equation we kept only the accumulation and convection terms for the x component of the velocity - as we already know, in CFD the variables to be computed are velocities; to make things even simpler, the coefficient of the first…

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    20 Apr 2020 12:59 AM IST

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    Prandtl Meyer Shock Flow

    Objective:

    Objective: The objective of this test is to simulate the steady-state airflow through a Prandtl Meyer Expansion Fan by using Converge CFD.    What is Shock Wave? Like an ordinary wave, a shock wave carries the energy and can propagate through a medium but is characterized by an abrupt, nearly discontinuous, change…

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    04 May 2020 02:45 AM IST

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    Steady state simulation of Flow of Air over a Throttle Body

    Objective:

    Objective: The objective of this project is to simulate the steady-state airflow through a throttle body by using Converge CFD.  Introduction: A throttle is a mechanism by which fluid flow is managed by constriction or obstruction. The term throttle has come to refer, informally, to any…

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    10 Apr 2020 02:36 AM IST

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    Flow Over an Airfoil

    Objective:

    Abstract: In this project, we are going to calculate the drag and lift coefficients for the NACA 2412 airfoil on four different angles of attacks i.e. 10, 50, 100, 150. Introduction: Airfoil is the cross-sectional shape of a wing, blade of a propeller, rotor, or turbine, or sail as seen in cross-section.…

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    26 Oct 2019 07:02 AM IST

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    Solving the steady and unsteady 2D heat conduction problem

    Objective:

    In this project, we will look to solve Steady and Unsteady 2D heat conduction problem using point iterative solvers such as JACOBI, Gauss-Seidel, Successive Over Relaxation (SOR) methods. For solving the Steady-state equation of 2D heat conduction: `(del^2T)/(delx^2)+(del^2T)/(dely^2)=0` Therefore by Central Differencing,…

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    30 Apr 2020 10:24 AM IST

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      PENDULUM MOTION

      Objective:

      WHAT ARE ODE( Ordinary Differential Equation)? In mathematics, an ordinary differential equation (ODE) is a differential equation containing one or more functions of one independent variable and the derivatives of those functions. The term ordinary is used in…

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      27 Apr 2020 02:07 AM IST

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        Effect of range of dx on first, second and fourth order approximations for a given value of x.

        Objective:

        What is Discretization? The general idea behind discretization is to break a domain into a mesh, and then replace derivatives in the governing equation with difference quotients. The discretization process is used to solve different PDE's, by changing them into algebraic terms.   Following code is written to…

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        04 May 2020 02:45 AM IST

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          Linear Convection

          Objective:

          LINEAR CONVECTION: This equation is the most accessible equation in CFD; from the Navier Stokes equation we kept only the accumulation and convection terms for the x component of the velocity - as we already know, in CFD the variables to be computed are velocities; to make things even simpler, the coefficient…

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          20 Apr 2020 01:50 PM IST

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          Taylor table method and Matlab code

          Objective:

            WHAT IS TAYLOR TABLE METHOD?  Taylor Table will determine the coefficients of the terms which minimizes the Taylor series error. It will also determine the Taylor series error and the order of accuracy of the method. In this case, Taylor Table method is used to determine the fourth-order approximations of the…

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          18 Apr 2020 05:39 AM IST

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          Flow Over Ahmed Body

          Objective:

          Objective: The objective of this project is to determine the Aerodynamic forces on the Ahmed body and Also to compare the velocity profile with experimental and computational data. What is an Ahmed Body? The Ahmed Body was first created by S.R. Ahmed in his research “Some Salient Features of the Time-Averaged Ground…

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          12 Mar 2020 05:59 AM IST

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            Simulation of Mixing tee and its Effectiveness

            Objective:

            Objective To simulate the flow of air through mixing tee and understand the effect of length of pipe and momentum ratio of velocity for mixing of air by using two different types of pipe i.e. short pipe and long pipe. About In industrial process engineering, mixing is a unit operation that involves…

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            21 Jun 2020 12:52 PM IST

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            Ahmed Body Challenge

            Objective:

            Objective: The objective of this project is to determine the Aerodynamic forces on the Ahmed body such as Drag and Lift coefficients and also to perform Grid Dependency test. What is an Ahmed Body? The Ahmed Body was first created by S.R. Ahmed in his research “Some Salient Features of the Time-Averaged Ground Vehicle…

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            26 Jul 2020 06:33 AM IST

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              Showing 1 of 17 projects

              1 Course Certificates

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              Advanced Aerodynamic Simulations using CONVERGE

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              2 Workshop Certificates

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              Find Your Ikigai with Operations and supply chain management

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              Value Analysis & Value Engineering

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