Finite difference gas-kinetic BGK scheme for compressible inviscid flow computation-Reference-Cited by-同舟云学术

Finite difference gas-kinetic BGK scheme for compressible inviscid flow computation

Published:2008-03 Issue:3 Volume:22 Page:183-192
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Omar Ashraf A.,Chit Ong J.,Hsuh Lim J.,Asrar Waqar

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

http://www.tandfonline.com/doi/pdf/10.1080/10618560701812824

Reference14 articles.

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

2. Development of an Improved Gas-Kinetic BGK Scheme for Inviscid and Viscous Flows

3. Ferziger, J.H. and Peric, M. 1996.Computational methods in fluid dynamics, 287–289. Germany: Springer.

4. Fottner, L., 1990. Test cases for computation of internal flows in aero engine components. Advisory group for aerospace research and development (AGARD), advisory report number 275, pp. 22–23.

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