EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING

EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING

<p align="justify">Composite material is a very effective material to replace metal because of light weight and also has good mechanical properties according to its aplication. Composite materials are used as components of commercial aircraft and military aircraft, for example over 5...

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Main Author: - NIM: 23616035 , Heriana
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/27836
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:27836
spelling id-itb.:278362018-08-28T15:27:02ZEXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING - NIM: 23616035 , Heriana Indonesia Theses INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/27836 <p align="justify">Composite material is a very effective material to replace metal because of light weight and also has good mechanical properties according to its aplication. Composite materials are used as components of commercial aircraft and military aircraft, for example over 50% composite material is used in aircraft 787. The study of ability of composite materials in resistance the load due to the blast impact is necessary. <br /> <br /> <br /> Blast Impact can be experimented explosion by using explosive material (TNT). This study was conducted to find out composite materials that have a good performance to be able to withstand the effects of blast explosion. The effect of explosion on the characteristics of composite materials is needed to uderstand.<p align="justify"> <br /> text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description <p align="justify">Composite material is a very effective material to replace metal because of light weight and also has good mechanical properties according to its aplication. Composite materials are used as components of commercial aircraft and military aircraft, for example over 50% composite material is used in aircraft 787. The study of ability of composite materials in resistance the load due to the blast impact is necessary. <br /> <br /> <br /> Blast Impact can be experimented explosion by using explosive material (TNT). This study was conducted to find out composite materials that have a good performance to be able to withstand the effects of blast explosion. The effect of explosion on the characteristics of composite materials is needed to uderstand.<p align="justify"> <br />
format Theses
author - NIM: 23616035 , Heriana
spellingShingle - NIM: 23616035 , Heriana
EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
author_facet - NIM: 23616035 , Heriana
author_sort - NIM: 23616035 , Heriana
title EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
title_short EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
title_full EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
title_fullStr EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
title_full_unstemmed EXPERIMEN STUDY OF FIBER REINFORCE POLYMER AND GLASS FIBER REINFORCE POLYMER COMPOSITE STRUCTURE OF IF-X AIRCRAFT UNDER BLAST LOADING
title_sort experimen study of fiber reinforce polymer and glass fiber reinforce polymer composite structure of if-x aircraft under blast loading
url https://digilib.itb.ac.id/gdl/view/27836
_version_ 1822922382971502592

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