A, Saket Chandra
(2016)
Development of a General-Purpose Compressible Flow AnuPravaha Based Solver using an Implicit Method (Fluids and Energy Systems).
Masters thesis, Indian Institute of Technology Hyderabad.
Abstract
With India focussing even more on Aerospace applications, research and development
in compressible
ow has received a boost in the country. We aim to
develop a general-purpose and robust compressible
ow solver to help in research
in Aerospace problems.
In this thesis we aim to develop a general-purpose and robust compressible
ow solver using the implicit MacCormack scheme infinite volume formulation. A
system of unsteady Navier-Stokes equations are integrated to a steady state solution
utilizing MacCormack's implicit numerical scheme. A new implicit boundary
treatment was introduced in the MacCormack implicit scheme. The scheme is unconditionally
stable and does not require solution of large systems of linear equations.
It is shown that the upgrade from explicit MacCormack scheme, previously
implemented in the solver, to an implicit one is very simple and straightforward.
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IITH Creators: |
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Item Type: |
Thesis
(Masters)
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Uncontrolled Keywords: |
supersonic flow, mach number, rarefield flow, coefficient of pressure, Drag, Temperature, TD716 |
Subjects: |
Physics > Mechanical and aerospace |
Depositing User: |
Team Library
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Date Deposited: |
25 Aug 2016 11:58 |
Last Modified: |
11 Jul 2019 11:38 |
URI: |
http://raiithold.iith.ac.in/id/eprint/2683 |
Publisher URL: |
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Related URLs: |
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