REVERSE ENGINEERING TERHADAP ANALISIS TEGANGAN BACK LADDER PESAWAT DHC-6 TWIN OTTER 300S DENGAN METODE ELEMEN HINGGA
Basically, a structure can accept a force and type of loading that varies with tolerable wear limits, because the force received can cause a structure to experience deformation to the failure of the structure. Likewise with the aircraft structure, it must be made strong in order to be able to withst...
Saved in:
Main Author: | SETYO DEWANTORO, (Author) |
---|---|
Format: | Book |
Published: |
2021-02-02.
|
Subjects: | |
Online Access: | Link Metadata |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
IMPROVEMENT DESIGN FRONT LADDER PESAWAT DHC - 6 TWIN OTTER 400S DALAM SEGI AERODINAMIS DAN KEKUATAN
by: Aji Farhan Utomo,
Published: (2021) -
Analisis Faktor Konsentrasi Tegangan Dengan Metode Elemen Hingga
by: Indratmo, Gege Prasetyo
Published: (2011) -
Analisis Uji Jatuh Badan Pesawat R80 Dengan Metode Elemen Hingga
by: Ardianto, Adik Nofa Rochma Wahyu, et al.
Published: (2016) -
ANALISIS TEGANGAN PADA FENDER KAPAL TIPE SETENGAH PIPA DENGAN FENDER TIPE M MENGGUNAKAN METODE ELEMEN HINGGA
by: Ikhwal Imam Rezaldy,
Published: (2022) -
Analisis Uji Tabrak Bodi Mobil Esemka dengan Metode Elemen Hingga
by: Darmawan, Agus, et al.
Published: (2016)