Splitting of Inviscid Fluxes for Real Gases

By: Nasa, National Aeronautics and Space Adm

Flux-vector and flux-difference splittings for the inviscid terms of the compressible flow equations are derived under the assumption of a general equation of state for a real gas in equilibrium. No necessary assumptions, approximations or auxiliary quantities are introduced. The formulas derived include several particular cases known for ideal gases and readily apply to curvilinear coordinates. Applications of the formulas in a TVD algorithm to one-dimensional shock-tube and nozzle problems show their quality and robustness. Liou, Meng-Sing and Vanleer, Bram and Shuen, Jian-Shun Glenn Research Center RTOP 505-62-21...

• Format: Paperback
• Language: English
• ISBN: 1728932203
• ISBN13: 9781728932200
• Release Date: January 1
• Publisher: Independently Published
• Length: 32 Pages
• Weight: 0.22 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"