Transonic Airfoil Flow Simulation. Part I: Mesh Generation and Inviscid Method
A calculation method for the subsonic and transonic viscous flow over airfoil using thedisplacement surface concept is described. Part I presents a mesh generation method forcomputational grid and a finite volume method for the time-dependent Euler equations. The inviscidsolution is used for the inv...
| Huvudupphovsmän: | , , , |
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| Materialtyp: | Artikel |
| Språk: | English |
| Publicerad: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2010-06-01
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| Serie: | INCAS Bulletin |
| Ämnen: | |
| Länkar: | http://bulletin.incas.ro/files/florin_frunzulica_v2no2_full.pdf |