PENGEMBANGAN MODUL ANALISIS BEBAN SIMETRIS PADA PESAWAT UDARA TRANSPOR SUBSONIK
The use of aircraft as a transportation mode is increased by time. Many aspects that need to be considered in the design process including aerodynamics, light weight structure, or other factors. Each aircraft that flies is subject to variation of structure load depending on the appropriate flight...
Saved in:
Main Author: | Wildan Agung Sanjaya, Yusuf |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/61656 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
PENGEMBANGAN MODUL ANALISIS BEBAN SIMETRIS PADA PESAWAT UDARA TRANSPOR SUBSONIK
by: Wildan Agung Sanjaya, Yusuf -
Perancangan sistem reduksi beban turbulensi udara pada struktur sayap pesawat terbang
by: Prihadana, Donny -
PENGEMBANGAN SUATU MODEL SIMETRI KIRI-KANAN DAN
IMPLIKASINYA
by: , Qidir Maulana Binu Soesanto, et al.
Published: (2011) -
Pembuatan dan Kalibrasi 5-Hole Probe dalam Medan Aliran Subsonik
by: DEWANAMPRIO, PANDU -
PENGEMBANGAN PERANGKAT LUNAK SIMULASI TERBANG PESAWAT UDARA MENGGUNAKAN JOYSTICK
by: Hernawati