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Penulis
:
ARIEF YUDHANTO (NIM 13697003)
Kontributor / Dosen Pembimbing
:
Pembimbing: Dr.Ir. Bambang K. Hadi
Jenis Koleksi
:
Tugas Akhir
Tahun Terbit
:
Penerbit
:
Fakultas
:
Subjek
:
Kata Kunci
:
panel buckling, sandwich panels, overall buckling
Sumber
:
Staf Input/Edit
:
Vika Anastasya Kovariansi
Ena Sukmana
File
:
7 file
Tanggal Input
:
09 Okt 2017
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2002 TA PP ARIEF YUDHANTO 1-COVER.pdf
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2002 TA PP ARIEF YUDHANTO 1-BAB 1.pdf
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2002 TA PP ARIEF YUDHANTO 1-BAB 2.pdf
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2002 TA PP ARIEF YUDHANTO 1-BAB 3.pdf
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2002 TA PP ARIEF YUDHANTO 1-BAB 4.pdf
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2002 TA PP ARIEF YUDHANTO 1-BAB 5.pdf
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2002 TA PP ARIEF YUDHANTO 1-PUSTAKA.pdf
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Ena Sukmana
Compressive loadings are inevitable in most aerospace structures, and buckling of panels in therefore of prime concern. One classical way in preventing this has been to use stiffeners of various shapes to reinforce structure's skin.
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