Transonic Airfoil Flow Simulation. Part I: Mesh Generation and Inviscid Method
Journal Title: INCAS BULLETIN - Year 2010, Vol 2, Issue 2
Abstract
A calculation method for the subsonic and transonic viscous flow over airfoil using the displacement surface concept is described. Part I presents a mesh generation method for computational grid and a finite volume method for the time-dependent Euler equations. The inviscid solution is used for the inviscid-viscous coupling procedure presented in the Part II.
Authors and Affiliations
Florin FRUNZULICA, , Horia DUMITRESCU, Alexandru DUMITRACHE, Vladimir CARDOS
Keywords
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- EP ID EP85502
- DOI 10.13111/2066-8201.2010.2.2.7
- Views 155
- Downloads 0
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