Aerodynamic Performance of NACA 662-015 Airfoil with Gurney Flap

Aerodynamic Performance of NACA 662-015 Airfoil with Gurney Flap

A numerical simulation was executed by using of ANSYS Fluent to demonstrate the effect of a Gurney flap (GF) on a National Advisory Committee for Aeronautics (NACA) 662-015 airfoil. The GFs are remarkable aerodynamic elements that show how a small modification to an airfoil’s trailing edge can have...

Full description

Saved in:
Bibliographic Details
Main Authors: Balram Mandal,  Roshani Kumari Gupta, Abhinav Adhikari, Biranchi Narayana Das, Atal Bihari Harichandan
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2024-12-01
Series:Journal of Aerospace Technology and Management
Subjects:
Reynolds number
GF
Lift augmentation
Drag reduction
Lift drag ratio
Online Access:https://jatm.com.br/jatm/article/view/1347
Tags: Add Tag
No Tags, Be the first to tag this record!

Internet

https://jatm.com.br/jatm/article/view/1347

Similar Items