Study of Airfoil Characteristics on NACA 4415 with Reynolds Number Variations
This study uses computational methods to analyze fluid flow characteristics NACA 4415 in ultra-low, low, and moderate Reynolds number categories. The turbulence model chosen is the standard k-ε. The ultra-low Reynolds number used is 5×103, while the Reynolds number for the low category is 4.17×104....
Saved in:
Main Author: | Waridho Iskandar, (Author) |
---|---|
Format: | Book |
Published: |
PRAISE WORTHY PRIZE,
2022-06-01.
|
Subjects: | |
Online Access: | Link Metadata |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
THE EFFECT OF THE SPLIT NACA 0015 AIRFOIL ON VARIATIONS IN REYNOLDS NUMBER
by: Muhammad Fari Satria,
Published: (2023) -
Effects of Leading-Edge Defects of the NACA 0015 Airfoil on Aerodynamic Performance with Various Reynolds Number
by: Ulfa Hanifah Nurhaliza, -
Published: (2023) -
ANALISIS SIMULASI EFISIENSI TURBIN ANGIN SUMBU HORIZONTAL AIRFOIL NACA 4415 MENGGUNAKAN BLADE ELEMENT MOMENTUM (BEM) DAN COMPUTATIONAL FLUID DYNAMICS (CFD)
by: Reva Mazini,
Published: (2021) -
NUMERICAL MODELLING OF NACA 0015 AIRFOIL UNDER THE EROSION CONDITION
by: Rayhan Fariansyah Billad,
Published: (2024) -
Studi Eksperimen Pengaruh Sudut Serang Terhadap Performa Turbin Angin Sumbu Horisontal NACA 4415
by: Susanto, Andi, et al.
Published: (2015)