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...

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Main Authors: Muharrem Özgün, Sinan Eyi
Format: Article
Language:English
Published: Turkish Air Force Academy 2014-07-01
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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author Muharrem Özgün
Sinan Eyi
author_facet Muharrem Özgün
Sinan Eyi
author_sort Muharrem Özgün
collection DOAJ
description 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 Jacobian matrix. Flow parameters and convective heat transfer are analyzed on Apollo AS-202 Space Capsule. Also, one-equation Spalart-Allmaras turbulence model is used to analyze hypersonic turbulent flow since this turbulence model is numerically robust and generally gives good predictions in hypersonic applications.
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spelling doaj.art-a6ef50e2e9ae48cf954b93ccc96f62062023-02-15T16:20:21ZengTurkish Air Force AcademyHavacılık ve Uzay Teknolojileri Dergisi1304-04481304-04482014-07-01727177ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONSMuharrem Özgün0Sinan Eyi1Middle East Technical UniversityMiddle East Technical UniversityThe 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 Jacobian matrix. Flow parameters and convective heat transfer are analyzed on Apollo AS-202 Space Capsule. Also, one-equation Spalart-Allmaras turbulence model is used to analyze hypersonic turbulent flow since this turbulence model is numerically robust and generally gives good predictions in hypersonic applications.http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/78/73Hypersonic FlowConvective Heat TransferTurbulence ModelingComputational Fluid Dynamics
spellingShingle Muharrem Özgün
Sinan Eyi
ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
Havacılık ve Uzay Teknolojileri Dergisi
Hypersonic Flow
Convective Heat Transfer
Turbulence Modeling
Computational Fluid Dynamics
title ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
title_full ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
title_fullStr ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
title_full_unstemmed ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
title_short ANALYSIS OF THREE DIMENSIONAL HYPERSONIC FLOW AROUND RE-ENTRY VEHICLE USING NAVIER-STOKES EQUATIONS
title_sort analysis of three dimensional hypersonic flow around re entry vehicle using navier stokes equations
topic Hypersonic Flow
Convective Heat Transfer
Turbulence Modeling
Computational Fluid Dynamics
url http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/78/73
work_keys_str_mv AT muharremozgun analysisofthreedimensionalhypersonicflowaroundreentryvehicleusingnavierstokesequations
AT sinaneyi analysisofthreedimensionalhypersonicflowaroundreentryvehicleusingnavierstokesequations