ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
The purpose of this study is to develop an accurate and efficient CFD code that can be used in hypersonic flows. The flow analysis is based on the three dimensional Navier-Stokes equations. These equations are solved by using Newton’s method and the analytical method is used to calculate the Jacobi...
Main Authors: | Muharrem Özgün, Sinan Eyi |
---|---|
Format: | Article |
Language: | English |
Published: |
Turkish Air Force Academy
2014-07-01
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Series: | Havacılık ve Uzay Teknolojileri Dergisi |
Subjects: | |
Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/78/73 |
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