Numerical Study of Variable Camber Continuous Trailing Edge Flap at Off-Design Conditions

Numerical Study of Variable Camber Continuous Trailing Edge Flap at Off-Design Conditions

Numerical simulations are performed to study the outboard airfoil of advanced technology regional aircraft (ATRA) wings with five different variable camber continuous trailing edge flap (VCCTEF) configurations. The computational study aims to improve the aerodynamic efficiency of the airfoil under c...

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Bibliographic Details
Main Authors: Mohammed Abdul Raheem, Prasetyo Edi, Amjad A. Pasha, Mustafa M. Rahman, Khalid A. Juhany
Format: Article
Language:English
Published: MDPI AG 2019-08-01
Series:Energies
Subjects:
variable camber continuous trailing edge flap
advanced technology regional aircraft wing
computational fluid dynamics
trailing edge flap
turbulence model
Online Access:https://www.mdpi.com/1996-1073/12/16/3185

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https://www.mdpi.com/1996-1073/12/16/3185

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