ANALISIS NUMERIK PENGARUH SLOT SUCTION DAN BLOWING JET TERHADAP KARAKTERISTIK ALIRAN UDARA DI SEKITAR AIRFOIL NACA 0012

Fatichah, Alfarel Muchammad Alif (2025) ANALISIS NUMERIK PENGARUH SLOT SUCTION DAN BLOWING JET TERHADAP KARAKTERISTIK ALIRAN UDARA DI SEKITAR AIRFOIL NACA 0012. Undergraduate thesis, UPN VETERAN JAWA TIMUR.

[img] Text (Cover)
21036010041.-cover.pdf

Download (2MB)
[img] Text (Bab 1)
21036010041.-BAB 1.pdf

Download (219kB)
[img] Text (Bab 2)
21036010041.-BAB 2.pdf
Restricted to Repository staff only until 8 December 2027.

Download (643kB) | Request a copy
[img] Text (Bab 3)
21036010041.-BAB 3.pdf
Restricted to Repository staff only until 8 December 2027.

Download (387kB) | Request a copy
[img] Text (Bab 4)
21036010041.-BAB 4.pdf
Restricted to Repository staff only until 8 December 2027.

Download (2MB) | Request a copy
[img] Text (Bab 5)
21036010041.-BAB 5.pdf

Download (190kB)
[img] Text (Daftar Pustaka)
21036010041.-daftarpustaka.pdf

Download (187kB)
[img] Text (Lampiran)
21036010041.-lampiran.pdf
Restricted to Repository staff only until 8 December 2027.

Download (858kB) | Request a copy

Abstract

This study aims to numerically analyze the effectiveness of Active Flow Control (AFC) using suction and blowing jet slots in improving the aerodynamic performance of the NACA 0012 airfoil. The main focus is to measure the increase in the lift coefficient (CL), the reduction in the drag coefficient (CD), and the stall delay at high angles of attack. The method used is Computational Fluid Dynamics (CFD) with variations in the angle of attack from 0o to 14o airspeed inlet 43,82, suction flow dan jet blowing (5 m/s to 15 m/s) as simulation conditions. The implementation of AFC is carried out on the boundary layer to manipulate the pressure and velocity distribution. The simulation results show that blowing jet is very effective in delaying stall and significantly increasing (CL)max. Meanwhile, suction serves to stabilize the boundary layer, contributing to aerodynamic efficiency. In conclusion, the combination of suction and blowing jet AFC is a proven strategy to optimize the lift to drag ratio (L/D), resulting in superior aerodynamic performance on the NACA 0012 airfoil

Item Type: Thesis (Undergraduate)
Contributors:
ContributionContributorsNIDN/NIDKEmail
Thesis advisorFaizin, Ahmad KhairulNIDN0020019302ahmad.khairul.tm.@upnjatim.ac.id
Subjects: Q Science > Q Science (General)
Divisions: Faculty of Engineering > Departement of Mechanical Engineering
Depositing User: Alfarel Muchammad Alif Fatichah
Date Deposited: 22 Dec 2025 04:40
Last Modified: 22 Dec 2025 05:03
URI: https://repository.upnjatim.ac.id/id/eprint/48174

Actions (login required)

View Item View Item