ANISOGRID WING STRUCTURE FLUTTER ANALYSIS ON JET FIGHTER AIRCRAFT BY USING MSC NASTRAN SOFTWARE
The fighter aircraft made must refer to the standard fighter aircraft structure so that the aircraft is safe and airworthy. The aircraft structure will be said to be safe if there is no failure phenomenon. Flutter is one of the instability phenomena due to the interaction of aerodynamic, inertia, an...
Saved in:
Main Author: | Arif Izzuddin, Mohammad |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/62002 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
ANISOGRID WING STRUCTURE FLUTTER ANALYSIS ON JET FIGHTER AIRCRAFT BY USING MSC NASTRAN SOFTWARE
by: Arif Izzuddin, Mohammad -
COMPUTATIONAL FLUTTER ANALYSIS ON WIND TUNNEL MODEL OF FIGHTER AIRCRAFT WING WITH CONVENTIONAL AND ANISOGRID STRUCTURAL CONFIGURATIONS
by: Rizqy Albana, Naufal -
OPTIMIZATION OF COMPOSITE WING STRUCTURE WITH STATIC, BUCKLING AND FLUTTER CONSTRAINT USING MSC NASTRAN
by: WIDIRAMDHANI, MARTINA -
FLUTTER ANALYSIS FIGHTER AIRCRAFT WING WITH CONVENTIONAL STRUCTURE CONFIGURATION
by: Hayati Putri, Mardiah -
FLUTTER ANALYSIS FIGHTER AIRCRAFT WING WITH CONVENTIONAL STRUCTURE CONFIGURATION
by: HAYATI PUTRI , MARDIAH