Effect of Vortex Generators on Airfoil NACA 632-415 to Aerodynamic Characteristics Using CFD
To determine the aircraft’s flight performance, the airfoil type must be considered when designing the wing. A vortex can form when the airfoil travels through a fluid stream with a difference in velocity and pressure around it. Airfoil modification is carried out to delay the occurrence of flow sep...
Main Authors: | Rosyida Permatasari, Gusty Widyawati |
---|---|
Format: | Article |
Language: | English |
Published: |
Universitas Riau
2023-02-01
|
Series: | International Journal of Electrical, Energy and Power System Engineering |
Subjects: | |
Online Access: | https://ijeepse.id/journal/index.php/ijeepse/article/view/136 |
Similar Items
-
The Effect of Location and Shape of Vortex Generators on Aerodynamic Characteristics of a NACA 4415 Airfoil
by: Khuder N. Abed
Published: (2023-10-01) -
Numerical and experimental study of the impact on aerodynamic characteristics of the NACA0012 airfoil
by: Molaa Ayat Abdulhussien, et al.
Published: (2024-02-01) -
Numerical Investigation of Winglet Aerodynamics and Dimple Effect of NACA 0017 Airfoil for a Freight Aircraft
by: Matthew Thomas Lewthwaite, et al.
Published: (2022-03-01) -
Control of Separation For NACA 2412 Airfoil At Different Angles of Attack Using Air Blowing
by: Jalal M. Jalil, et al.
Published: (2010-08-01) -
The effect of the blowing and suction from one or two positions over the suction surface of NACA0012 airfoil on aerodynamic performance in turbulent flow
by: Pooria Akbarzadeh, et al.
Published: (2017-12-01)