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Hasil Pencarian

Ditemukan 8 dokumen yang sesuai dengan query
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Koln: Taschen, 2011
R 747 INT
Buku Referensi  Universitas Indonesia Library
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Harmon, Sharon Koomen
New York: John Wiley & Sons, 2001
R 343.73 Har c
Buku Referensi  Universitas Indonesia Library
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New York: Visual Reference Pub. Inc., 2003
725.23 COR
Buku Teks SO  Universitas Indonesia Library
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Vidiella, Alex Sanchez
Beverly: Quayside, 2008
R 729 VID a
Buku Referensi  Universitas Indonesia Library
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Massachusetts: Rockport Publishers, 1998
747.885 HOT (1);747.885 HOT (2)
Buku Teks SO  Universitas Indonesia Library
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Hasegawa, Noriyoshi
Singapore: Page one publishing pte ltd, 2010
741.24 HAS s
Buku Teks SO  Universitas Indonesia Library
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McDermatt, Catherine
"Design Museum: Contemporary Design" presents a collection of the most important and influential pieces of design produced in modern times. Featuring the defining work of such pioneers as Frank Lloyd Wright, Rem Koolhaas, Gio Ponti, Eileen Gray, Christian Dior, Marc Jacobs, Saul Bass, Philippe Starck, Neville Brody, Jasper Morrison and many others, the result is a celebration of the artistic diversity of recent decades. With a selection of nearly 400 of the best and most enduring examples of modern design, including the very latest examples from the twenty-first century, "Design Museum: Contemporary Design" is an informative and colourful survey of the entire genre, from advertising and architecture, to fashion and furniture, and transport and type, via communications, interiors, lighting, household items and products. "Design Museum: Contemporary Design" is an essential reference work for students, designers in all fields and anyone interested in innovative and intelligent design."--Publisher desc"
London : Carlton, 2010
745.44 MCD c
Buku Teks SO  Universitas Indonesia Library
cover
Tyana Charity Sanjaya
"Studi ini meneliti pengaruh filler woven fiberglass terhadap sifat mampu bentuk dan ketahanan benturan lembaran komposit sandwich SS 304/SS 304 wire mesh/SS 304, yang dirancang untuk aplikasi interior pesawat terbang. Komposit dibuat dengan mengapit lapisan wire mesh SS 304 di antara dua lembar SS 304, dengan integrasi filler woven fiberglass. Penilaian kemampuan bentuk, termasuk stretching (LDH), uji stretch-bend, dan hole expansion, mengungkapkan bahwa penggabungan filler fiberglass meningkatkan kemampuan bentuk, sebagaimana dibuktikan dengan peningkatan LDH menjadi 8,8 mm dibandingkan dengan 6 mm untuk komposit tanpa filler. Rasio stretch-bend sebagian besar tidak terpengaruh, dengan nilai 11,834 dan 11,976 untuk kedua konfigurasi, yang menunjukkan bahwa pola anyaman fiberglass terutama meningkatkan ketahanan delaminasi. Pengujian hole expansion menunjukkan peningkatan marjinal pada ketahanan retak tepi, dengan peningkatan rasio hole expansion menjadi 4% dari 3,8% ketika filler digunakan. Dari pengujian impak diketahui peningkatan yang signifikan dalam penyerapan energi untuk komposit yang mengandung filler fiberglass, yang ditunjukkan dengan peningkatan disipasi energi impak menjadi 6 J dari 4,2 J. Peningkatan ketahanan impak ini sangat penting untuk meminimalkan risiko kegagalan akibat benturan mendadak pada interior pesawat. Dari studi ini dapat disimpulkan bahwa penambahan filler woven fiberglass pada komposit sandwich SS 304/SS 304 wire mesh/SS 304 meningkatkan sifat mampu bentuk dan ketahanan impak, sehingga cocok untuk aplikasi interior pesawat. Penelitian lebih lanjut direkomendasikan untuk mengoptimalkan proses fabrikasi dan menilai kinerja dalam berbagai kondisi.

This study examines the influence of woven fiberglass filler on the formability and impact resistance of SS 304/SS 304 wire mesh/SS 304 sandwich composite sheets, tailored for aircraft interior applications. The composites are fabricated by sandwiching a layer of SS 304 wire mesh between two SS 304 sheets, with the integration of woven fiberglass filler. Formability assessments, including limiting dome height (LDH), stretch-bend, and hole expansion tests, reveal that incorporating fiberglass filler enhances formability, as evidenced by an increase in LDH to 8.8 mm compared to 6 mm for composites without filler. The stretch-bend ratio remains largely unaffected, with values of 11.834 and 11.976 for both configurations, indicating that the fiberglass weave pattern primarily enhances delamination resistance. Hole expansion tests show a marginal increase in edge cracking resistance, with an increase in hole expansion ratio to 4% from 3.8% when the filler is used. Impact testing highlights a significant improvement in energy absorption for composites containing the fiberglass filler, demonstrated by an increase in impact energy dissipation to 6 J from 4.2 J. These improvements in impact resistance are crucial for minimizing failure risks due to sudden impacts in aircraft interiors. The study concludes that the addition of woven fiberglass filler to SS 304/SS 304 wire mesh/SS 304 sandwich composites substantially improves both formability and impact resistance, making them well-suited for airplane interior applications. Further research is recommended to optimize the fabricatio"
Depok: Fakultas Teknik Universitas Indonesia, 2024
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UI - Skripsi Membership  Universitas Indonesia Library