OPTIMISASI STRUKTUR STIFFENED PANEL PADA KULIT SAYAP PESAWAT âWHALEâ DENGAN KRITERIA LOCAL BUCKLING DAN GLOBAL BUCKLING
Stiffened panel is an effective structure in resisting buckling loads. Its failure modes is quite complicated because there are so many dimensional parameters and different buckling modes. Some of them are the local buckling, flexural buckling, torsional buckling, inter-rivet buckling and wrinkling....
Saved in:
Main Author: | Ikhsan, Muhammad |
---|---|
Format: | Theses |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/33364 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
OPTIMASI GEOMETRI STIFFENER DAN SUSUNAN LAMINAT KOMPOSIT PADA STIFFENED PANEL DENGAN KRITERIA BUCKLING UNTUK PERANCANGAN KULIT SAYAP ATAS PESAWAT âWHALEâ
by: Kurniawan Silalahi, Irvan -
PERANCANGAN STRUKTUR KOMPOSIT LAMINATE PADA UPPER WING SKIN PESAWAT âWHALEâ DENGAN KRITERIA TSAI-HILL DAN BUCKLING
by: Ikhsan, Muhammad -
OPTIMASI BUCKLING KOMPOSIT STIFFENED PANEL âBLADE STIFFENERâ
by: Kuswoyo, Andi -
Local Buckling of Stiffened Plates in Offshore Structures
by: Shanmugam, N.E., et al.
Published: (2014) -
ANALISIS DAN OPTIMASI STRUKTUR ANISOGRID KOMPOSIT SAYAP PESAWAT TEMPUR DENGAN KRITERIA KEGAGALAN STATIK, BUCKLING DAN FLUTTER MENGGUNAKAN METODE ELEMEN HINGGA
by: Muhammad Naufal Ramadhan, Teuku