OBJECTIVE OF THE CHALLENGE: Objective of the challenge is to simulate the isentropic flow through a 1D subsonic-supersonic nozzle by deriving the governing (continuity,momentum and energy) equations in both conserved and non conserved form using Maccormack's technique. Governing equations in non conservative form : continuity…
Naveenkumar Aavula
updated on 21 Jul 2020
Project Details
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Read more Projects by Naveenkumar Aavula (11)
Conjugate Heat Transfer Analysis on a graphics card.
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23 Dec 2020 02:52 PM IST
Exhaust Port Challenge
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29 Oct 2020 03:08 PM IST
Flow over a backward facing step with different grading factors
OBJECTIVE: The main objective of the challenge is to simulate the flow over a backward facing step with grading factors 0.2,0.5 and 0.8 and to compare the velocity magnitude contours also to observe the changes in the velocity magnitude profile as a function of mesh grading factor ,measured at 0.085m from the inlet for…
26 Oct 2020 06:39 AM IST
Ahmed Body Challenge
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17 Oct 2020 08:24 AM IST
Steady Vs Unsteady flow over a cylinder
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12 Sep 2020 09:25 AM IST
Mixing efficiency
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27 Aug 2020 03:50 AM IST
Week 3 - Taylor table method and Matlab code
OBJECTIVE OF CHALLENGE: To derive the central,right skewed and left skewed schemes for given function of second order derivative and fourth order approximation using taylor table also to plot the error values for a range of dx Calculating the number of equations to be considered for taylor table N=A+B-1; for central…
05 Aug 2020 02:57 AM IST
Week 9 - FVM Literature Review
Finite volume method:Finite volume method is a domain discretization technique used alternatively to finite difference method and finite element method where small volume surrounding a grid point in control volumes is discretized and solved for the governing equations. It solves governing equtions in the integral form…
02 Aug 2020 08:47 AM IST
Week 7 - Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method
OBJECTIVE OF THE CHALLENGE: Objective of the challenge is to simulate the isentropic flow through a 1D subsonic-supersonic nozzle by deriving the governing (continuity,momentum and energy) equations in both conserved and non conserved form using Maccormack's technique. Governing equations in non conservative form : continuity…
21 Jul 2020 03:56 AM IST
Week 5 - Mid term project - Solving the steady and unsteady 2D heat conduction problem
RESULTS AND DISCUSSION: The given problem is solved using 'Jacobi ,gauss siedal and successive over relaxation methods',for steady and transient states. For discretizing the 2D heat conduction, we are employing the 'Central differencing scheme' as it is more accurate than the skewed schemes. In the 'steady…
12 Jun 2020 04:08 AM IST