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Shubham Sawarkar

Skills Acquired at Skill-Lync :

  • CFD
  • AERODYNAMICS
  • CONVERGE-CFD

11 Projects

Flow over a backward facing step in CONVERGE CFD

Objective:

Objective To simulate and analyse 2D open channel flow for backward facing step for 3 different mesh size for same geometry and same initial condition for 3 different cases. Case 1: dx = 2e-3m,              dy = 2e-3m,       dz = 2e-3m Case 2: dx = 1.5e-3m, …

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17 Nov 2019 04:26 PM IST

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    Conjugate Heat Transfer Simulation

    Objective:

    Objective To Simulate and analyse conjugate heat transfer flow through circular pipe.  Problem Description A flow through pipe having internal diameter 0.03 mm and thickness of 0.005 mm is considered made up of aluminium is considered.The inlet Reynolds Number is 7000. Through outerwall of there is heat flux of -…

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    17 Nov 2019 04:26 PM IST

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      Prandtl Meyer Shock problem

      Objective:

      Objective To simulate and analyse Prandtl Meyer Shock flow Problem. In this case we have considered 2 cases. Case A : Initial velocity in region is supersonic (680 m/s) at 1 atm Pressure @ 300 K Case B : Initial velocity in region is subsonic (100 m/s) at 1 atm Pressure @ 300 K each case is simulated over 3 different…

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      17 Nov 2019 04:26 PM IST

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        FSAE Car Project

        Objective:

        Objectives To simulate and analyse flow over FSAE car for two cases Case 1:  Racing track conditions - Lot of turns Average lap speeds - 45kmph 70% turns at 45 degrees 20% turns at 80 degrees 10% turns at 20 degrees Case 2: Racing track conditions - Straights Average lap speed - 75kmph  Problem Description  …

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        01 Dec 2019 07:38 AM IST

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          Channel flow simulation using CONVERGE CFD

          Objective:

          Objective To simulate and analyse 2D open channel flow for 3 different mesh size for same geometry and same initial condition. Case 1: dx = 2e-4m,              dy = 2e-4m,       dz = 2e-4m Case 2: dx = 1.5e-4m,           dy = 1.5e-4m, …

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          17 Nov 2019 04:26 PM IST

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            Transient simulation of flow over a throttle body

            Objective:

            Objective To simulate and analye flow over throttle body under Transient state condition. Here, for analysis we have considered total 5 cases using Transient solver. Case 1 : Pipe Flow Case 2 : No Throttle Case 3 : Throttle at 0 degree. Case 4 : Throttle at 25 degree. Case 5 : Throttle moving from 0…

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            17 Nov 2019 04:26 PM IST

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              NACA 2412 Airfoil

              Objective:

              Objectives To simulate and analyse flow over NACA 2412 Airfoil and calculate drag and lift coefficients for different angle of attack as follows. Angle of attack = 1º Angle of attack = 5º Angle of attack = 10º Angle of attack = 15º also to simulate for different Turbulence model k-ω -sst RNG -k-ϵ…

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              03 Dec 2019 10:17 AM IST

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                Shock tube simulation

                Objective:

                Objective To Simulate and analyse flow through tube which occurs because of shock takes place in the tube due to suddent mixing of the two species kept at two different pressure. Problem Description A closed tube is considered in which the half part is occupied by N2 at 600000  pa and half part is occupied by O2 at …

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                17 Nov 2019 04:26 PM IST

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                  Steady state simulation of flow over a throttle body

                  Objective:

                  Objective To simulate and analye flow over throttle body under steady state condition. Here, for analysis we have considered total 4 cases. Case 1 : Straight Pipe Flow Case 2 : No Throttle  Case 3 : Throttle at 0 degree. Case 4 : Throttle at 25 degree. Geometry The link for .stl file of geometry…

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                  17 Nov 2019 04:26 PM IST

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                    Modeling and Simulation of flow around an Ahmed Body

                    Objective:

                    Objectives To simulate and analyse flow over an ahmed body  To calculate Lift and Drag force coefficients Problem Description     The geometrical shape of the Ahmed body investigated is depicted in Figure 1 for inlet bulk velocity of 40 m/s. The body represents the basic aerodynamic properties of a…

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                    02 Dec 2019 07:19 AM IST

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                      RANS derivation and analysis

                      Objective:

                      https://drive.google.com/open?id=1Er66WkvEOKPwH5NPnBv8MR3zp6mqbr1g

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                      17 Nov 2019 04:26 PM IST

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