Near Stall Unsteady Flow Responses to Morphing Flap Deflections

Near Stall Unsteady Flow Responses to Morphing Flap Deflections

The unsteady flow characteristics and responses of an NACA 0012 airfoil fitted with a bio-inspired morphing trailing edge flap (TEF) at near-stall angles of attack (AoA) undergoing downward deflections are investigated at a Reynolds number of 0.62 × 10<sup>6</sup> near stall. An unsteady...

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Bibliographic Details
Main Authors: Chawki Abdessemed, Yufeng Yao, Abdessalem Bouferrouk
Format: Article
Language:English
Published: MDPI AG 2021-05-01
Series:Fluids
Subjects:
morphing
bioinspiration
dynamic mesh
RANS-LES
stress-blended eddy simulation (SBES)
computational fluid dynamics (CFD)
Online Access:https://www.mdpi.com/2311-5521/6/5/180

Internet

https://www.mdpi.com/2311-5521/6/5/180

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