Atmosferik geçiş yapan araç etrafında navier- stokes denklemleri ile üç boyutlu hipersonik akış analizi

Date

2014-06-01

Author

Özgün, Muharrem
Eyi, Sinan

Metadata

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Bu çalışmada hipersonik akışlar için kullanılabilecek isabetli ve etkin bir hesaplamalı akışkanlar dinamiği kodu geliştirilmesi amaçlanmaktadır. Akış analizi üç boyutlu Navier-Stokes denklemlerini temel almaktadır. Bu denklemler Newton metoduyla çözülmekte ve Jacobian matrislerini hesaplamak için analitik metot kullanılmaktadır. Model olarak alınan AS-202 Apollo uzay aracı geometrisi üzerinde akış parametreleri ve taşınımla ısı transferi analiz edilecektir. Ayrıca nümerik olarak stabil olan ve genelde hipersonik akış uygulamalarında iyi tahminler sağlayan Spalart-Allmaras türbülans modeli kullanılarak hipersonik akış için türbülanslı akış analizi yapılacaktır.

Subject Keywords

Hipersonik akış, Taşınımla Isı transferi, Türbülans modellemesi, Hesaplamalı akışkanlar dinamiği, Hypersonic flow, Convective heat transfer, Turbulence modeling, Computational fluid dynamics

URI

https://hdl.handle.net/11511/74498

Journal

Havacılık ve Uzay Teknolojileri Dergisi

Collections

Department of Aerospace Engineering, Article

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Citation Formats

M. Özgün and S. Eyi, “Atmosferik geçiş yapan araç etrafında navier- stokes denklemleri ile üç boyutlu hipersonik akış analizi ,” Havacılık ve Uzay Teknolojileri Dergisi, pp. 71–77, 2014, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/74498.