SHAPE OPTIMIZATION OF GLIDER WING GL-1 USING CFD ADJOINT SOLVER METHOD
Adjoint method is one of computational fluid dynamic-based optimization tools for optimizing the aerodynamic shape of the body. The method is rarely used in aircraft because it still in development process. However, this research attempt to use adjoint method on optmizing GL-1 Glider which is the fi...
Saved in:
Main Author: | Ahmad Maulana, Faridl |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/42250 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
GLIDER GL-1 WING STRUCTURE ANALYSIS
by: Tanoyo, Kalvin -
ANALYSIS OF STABILITY DYNAMIC AEROELASTIC OF GLIDER GL-1 WING USE FINITE ELEMENT METHOD
by: Khoirun Nisa (13614073), Anis -
INTERNAL CONFIGURATION DESIGN OF GLIDER GL-1
by: Fikri Zulkarnain, Muhammad -
CONCEPTUAL DESIGN OF INDONESIAN NATIONAL GLIDER GL-01
by: AJI PRATAMA, HENDI -
CONCEPTUAL DESIGN OF INDONESIAN NATIONAL GLIDER GL-01
by: Aji Pratama, Hendi