Effects of leading-edge defects of the NACA 0015 airfoil on aerodynamic performance with various Reynolds number
This study investigates and identifies the effects produced by defect on an airfoil when compared to a smooth airfoil. The defect used in this research is of the surface concaved defect (SDD) type, with a deep defect characterized by a smooth sunken deformation. The opening size used is t*=12%, and...
Saved in:
Main Authors: | Ulfa Hanifah Nurhaliza, James Julian, Fitri Wahyuni, Waridho Iskandar |
---|---|
Format: | Article |
Language: | English |
Published: |
University of Muhammadiyah Malang
2023-12-01
|
Series: | JEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering) |
Subjects: | |
Online Access: | https://ejournal.umm.ac.id/index.php/JEMMME/article/view/29400 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
GAYA ANGKAT DAN GAYA HAMBAT SAYAP PUNA MODEL NACA 0015 MENGGUNAKAN SIMULASI ANSYS FLUENT
by: Muhammad Dzulfikar, et al.
Published: (2024-12-01) -
Enhanced aerodynamic performance of NACA4412 airfoil through integrated plasma actuator and Gurney flap flow control
by: K.V. Karthikeyan, et al.
Published: (2025-03-01) -
Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds
by: Sinan Fidan, et al.
Published: (2022-12-01) -
The Effect of Microcylinder Shape on Enhancing the Aerodynamics of Airfoils at a Low Reynolds Number
by: Renata Gnatowska, et al.
Published: (2024-12-01) -
Multi-slotted airfoil design for enhanced aerodynamic performance and economic efficiency
by: Mohamed A. Aziz, et al.
Published: (2025-02-01)