Application of Gas-Kinetic BGK Scheme for Solving 2-D Compressible Inviscid Flow around Linear Turbine Cascade

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Application of Gas-Kinetic BGK Scheme for Solving 2-D Compressible Inviscid Flow around Linear Turbine Cascade

Fluid flows within turbomachinery tend to be extremely complex. Understanding such flows is crucial in the effort to improve current turbomachinery designs. Hence, computational approaches can be used to great advantage in this regard. In this paper, gas-kinetic BGK (Bhatnagar-Gross-Krook) scheme is...

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Bibliographic Details
Main Authors:	Abdusslam, Saleh N., Ong, Jiunn Chit, Hamdan, Megat M., Omar, Ashraf Ali, Asrar, Waqar
Format:	Article
Language:	English
Published:	Taylor & Francis 2006
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/5976/ http://irep.iium.edu.my/5976/5/waqar_15502280600826357.fp.png_v03.pdf

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