Three dimensional hypersonic flow analysis around a reentry vehicle using navier‐stokes equations

Date

2016-07-11

Author

Özgün, Muharrem
Eyi, Sinan

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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/Newton-Gmres method. The analytical method is used to calculate the Jacobian matrix. Flow parameters and convective heat transfer are analyzed on Apollo AS-202 Command Module. Also, algebraic Baldwin-Lomax turbulence model and one-equation Spalart-Allmaras turbulence model is used to analyze hypersonic turbulent flow

Subject Keywords

Computational Fluid Dynamics (CFD), Hypersonic flow, Turbulence modeling, Newton/Newton-Gmres method

URI

http://iccfd9.itu.edu.tr/assets/pdf/papers/ICCFD9-2016-299.pdf
https://hdl.handle.net/11511/86903

Conference Name

Ninth International Conference on Computational Fluid Dynamics (ICCFD9), 11 - 15 Temmuz 2016

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

M. Özgün and S. Eyi, “Three dimensional hypersonic flow analysis around a reentry vehicle using navier‐stokes equations,” Istanbul, Turkey, 2016, vol. 9, Accessed: 00, 2021. [Online]. Available: http://iccfd9.itu.edu.tr/assets/pdf/papers/ICCFD9-2016-299.pdf.