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The governing equations for the boundary layers are the Navier Stokes equation shown below: ∂u∂x+∂v∂y=0 - Continuity Equation ρ(∂u∂t+u∂u∂x+v∂u∂y)=−dρdx+μ∂2u∂y2 - Momentum Equation `rhoc((delT)/(delt) + u(delT)/(delx) + v(delT)/(dely))=…
Naga Venkata Sai Jitin Jami
updated on 28 Jul 2019
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Week 7 - Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method
Objective : Numerical simulation of 1D supersonic nozzle flow using Macormack Method using conservative and non-conservative forms of equation Assumptions: 1. Flow inside the nozzle is assumed to be isentropic. 2. The flow is considered Quasi-1D as properties vary along the x axis and not the y axis. 3. Compreesibe flow…
18 Mar 2021 08:09 PM IST
Calculation of AFT in constant pressure and constant volume condition
1. Effect of Equivalence Ratio on Adiabatic Flame Temperature The python program was written to calculate AFT using Newton-Raphson Optimisation of the following function : f = (Enthalpy of products) - (Enthalpy of reactants) - R*((Number of moles of reactants)*T_stp - (Number of moles of products*T_ad) = 0 (Refer…
12 May 2020 01:35 AM IST
Transient Simulation of flow over a throttle body
Objective: To simulate flow through an elbow pipe with a throttle valve inside. This is a transient simulation as the valve inside will be moving. Procedure: A CAD model of the elbow joint with a throttle valve is imported into converge studio. A design disgnosis is run for any errors. Boundaries were flagged according…
12 May 2020 01:34 AM IST
Shock Tube Simulation
Objective: Perform a shock tube simulation to detect shock waves formed due to bursting of a membrane that seperates a high pressure region and a low pressure region. The intention is to provide the following: Mesh refinement profile based on gradient (Adaptive-Mesh Refinement) Pressure profile Temperature Profile Velocity…
12 May 2020 01:34 AM IST
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