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
Related Articles
- EP ID EP85502
- DOI 10.13111/2066-8201.2010.2.2.7
- Views 154
- Downloads 0
Academician Elie Carafoli
Airline Applications of Business Intelligence Systems
Airline industry is characterized by large quantities of complex, unstructured and rapid changing data that can be categorized as big data, requiring specialized analysis tools to explore it with the purpose of obtaining...
Present and potential security threats posed to civil aviation
Aircraft presents ideal object for terrorist attack. Apart from the risks posed by possible terrorist attacks on airborne aircraft, air terrorism includes the threats to general aviation on the ground, including airports...
BOOK REVIEWS: Numerical Methods in Fluid Dynamics (Metode Numerice in Dinamica Fluidelor), Sterian DANAILA, Corneliu BERBENTE Published by Editura Academiei Romane, Bucuresti, 2003, ISBN 973-27-0958-8
Nanofilled EPDM composite for aerospace applications
O-rings are designed to be seated in a groove and compressed during assembly between two or more parts, creating a seal at the interface. The joint may be static, or (in a few circumstances) may have relative motion betw...