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- Title
AERODYNAMIC CHARACTERISTICS OF AIRFOIL WITH SINGLE SLOTTED FLAP FOR LIGHT AIRPLANE WING.
- Authors
Damianov Todorov, Michael
- Abstract
A numerical study was performed on a NACA 23012 airfoil with a single slotted flap to examine the aerodynamic coefficients at Reynolds number of 3x106, and for help to identifying the forces acting on a light airplane wing. Besides, in the paper the flow fields around the airfoil with single slotted flap were shown. All calculations were made using a CFD code Fluent. For a turbulent model the Spalart-Allmaras method was chosen. Conclusions were made about the aerodynamic efficiency of the proposed configuration wing-single slotted flap.
- Publication
Scientific Research & Education in the Air Force - AFASES, 2015, Vol 2, p509
- ISSN
2247-3173
- Publication type
Academic Journal