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"High Performance Fiber Reinforced Cement Composites (HPFRCC) represent a class of cement composites whose stress-strain response in tension undergoes strain hardening behaviour accompanied by multiple cracking, leading to a high strain prior to failure. The primary objective of this International Workshop was to provide a compendium of up-to-date information on the most recent developments and research advances in the field of HPFRCC. Approximately 65 contributions from leading world experts are assembled in these proceedings and provide an authoritative perspective on the subject. Special topics include fresh and hardening state properties, self-compacting mixtures, mechanical behavior under compressive, tensile, and shear loading, structural applications, impact, earthquake and fire resistance, durability issues, ultra-high performance fiber reinforced concrete, and textile reinforced concrete. "

"Optical microscopy is one of the most valuable?but under utilized?tools for analyzing fiber reinforced polymer matrix composites. This hands-on instructional book covers everything; sample preparation, microscopic techniques, and applications. The power of optical microscopy to study the microstructure of these heterogeneous, anisotropic materials is illustrated with over 180 full color images."

"The purpose of this paper is to analyse the thermal conductivity of carbon/basalt fiber reinforced hybrid composite structures based on stacking sequences. The paper also investigates the thermal impedance of carbon fiber reinforced polymer (CFRP) and basalt fiber reinforced polymer (BFRP) with increased thickness. Research involved processing hybrid composite by using injection moulding. The weight ratios of fibers to polymers was 60%: 40%. Testing was conducted using the ASTM D 5470 standard test method. Results show that the stacking sequences of carbon/basalt fibers have a significant impact on thermal conductivity. Hybrid composite with the stacking sequence mode C3B4C3 has the lowest thermal conductivity at 0.187 W/mK, and the highest thermal impedance of 0.0052 m2K/W. The highest thermal impedance of BFRP is at 0.007 m2K/W with 2.5 mm thickness. In CFRP, the highest thermal impedance is achieved by 3.4 mm thickness with 0.005 m2K/W. Results therefore show that carbon/basalt/epoxy hybrid composites are good insulators, since thermal conductivity is less than 0.42 W/moK standard."

"Batang kelapa sawit merupakan limbah industri kelapa sawit yang melimpah. Salah satu pemanfaatan batang kelapa sawit yaitu untuk bahan campuran pembuatan papan semen. Papan semen berpenguat serat batang kelapa sawit dari penelitian ini ditujukan untuk penyerap suara. Penelitian ini bertujuan untuk mengevaluasi perlakuan awal terbaik terhadap serat batang kelapa sawit atau Oil Palm Trunk Fiber (OPTF) untuk meningkatkan kompatibilitas terbaik dengan bahan semen sehingga dihasilkan papan semen untuk penyerap suara dengan kinerja yang baik. Metode penelitian berfokus pada perlakuan pendahuluan terhadap OPTF, tambahan akselerator (CaCl2 3% dari berat semen) dan komposisinya dengan semen untuk menghasilkan papan semen. Perlakuan awal ini berupa perendaman air dingin pada suhu kamar selama 24 jam (OPTF-2) dan perlakuan karbonisasi hidrotermal pada suhu 130°C selama 4 jam (OPTF-3), serta tanpa perlakuan (OPTF-1). Komposisi serat dan semen yang digunakan yaitu 1 : 2,75; 1 : 3,00 dan 1 : 3,25 (basis berat). Hasil penelitian menunjukkan bahwa secara umum perlakuan terbaik untuk mendapatkan papan semen berpenguat OPTF dengan tujuan penyerap suara pada penelitian ini adalah perlakuan OPTF-3 dengan komposisi serat dan semen 1 : 2,75. Papan ini optimum digunakan sebagai papan penyerap suara pada frekuensi 4000 Hz. Nilai koefisien absorpsi (α) yang diperoleh sebesar 0,91

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Oil palm trunk is waste from oil palm industry that abundantly available. One of the uses of oil palm trunks is as mixtures to produce mixtures of cement boards. Palm fiber reinforced cement board from this research was intended for sound absorbtion. This study aimed to analyze the best pretreatment of oil palm trunk fiber (OPTF) to improve the best compatibility with cement materials for producing cement boards for good performance of sound absorbtion. The research method focused on the pre-treated OPTF with the addition of accelerator (CaCl2, 3% by weight of cement) and its composition with cement to produce cement board. This pre-treatment involved cold water immersion at room temperature for 24 hours (OPTF-2) and hydrothermal carbonization treatment at 130°C for 4 hours (OPTF-3); as well as fibre without pre-treatment (OPTF-1). The compositions of fiber and cement were 1: 2.75; 1: 3.00 and 1: 3.25 (weight base). In general, the results showed the best cement board with OPTF-3 fibre and cement composition of 1 : 2.75. The OPTF-3 reinforced cement board worked optimally for a sound absorbtion board at the frequency of 4000 Hz. The absorption coefficient (α) obtained is 0.91"

"The use of fiber-reinforced polymer (FRP) composite materials has had a dramatic impact on civil engineering techniques over the past three decades. FRPs are an ideal material for structural applications where high strength-to-weight and stiffness-to-weight ratios are required. Developments in fiber-reinforced polymer (FRP) composites for civil engineering outlines the latest developments in fiber-reinforced polymer (FRP) composites and their applications in civil engineering.Part one outlines the general developments of fiber-reinforced polymer (FRP) use, reviewing recent advancements in the design and processing techniques of composite materials. Part two outlines particular types of fiber-reinforced polymers and covers their use in a wide range of civil engineering and structural applications, including their use in disaster-resistant buildings, strengthening steel structures and bridge superstructures."

"This book examines current issues of fiber reinforced polymer (FRP) composites in civil infrastructure. The contents of this book are divided into two parts. The first part engages topics related to durability and service life of FRP composites and how they contribute to sustainability. The second part highlights implementation and applications of the FRP composites with an emphasis on bridge structures. An introductory chapter provides an overview of FRP composites and its role in a sustainable built environment highlighting the issues of durability and service life followed by a current review of sustainability in infrastructure design.​"

"Roket adalah kendaraan peluncur yang mampu mengangkut muatan ke tujuan yang diinginkan. Nosel merupakan komponen struktural terberat, yaitu menyumbang sekitar 30 % dari berat keseluruhan struktur roket sehingga sangat terbuka kemungkinan untuk mereduksi beratnya, dalam mendesain nosel juga harus memperhatikan beban mekanik dan termal yang cukup tinggi akibat dari pembakaran propelan untuk menghasilkan gaya dorong (thrust) roket. Salah satu alternatif untuk mereduksi berat adalah penggunaan material Komposit Polimer Berpenguat Serat Karbon, untuk mengaplikasikan material komposit tersebut terhadap nozzle case, perlu dilakukan karakterisasi sifat-sifat mekanik. Salah satu pengujian yang paling sering dilakukan yaitu uji tarik (tensile test), pengujian ini memiliki fungsi untuk mendapatkan nilai kekuatan, modulus elastisitas, dan failure mode. Pengujian Tarik dilakukan melalui dua tahapan untuk menyeleksi material yang mampu menerima beban termal. Pengujian tarik tahap pertama dilakukan dengan rentang temperatur dari RT sampai 200°C menggunakan mesin Shimadzu AG-50KNX PLUS Machine untuk seleksi material antara komposit C/LY5052 dengan C/ARMC berdasarkan ketangguhan pada temperature yang diuji. Selanjutnya material yang terpilih diteruskan ke pengujian tahap dua, dimana material terpilih di uji Tarik pada rentang temperatur RT sampai 800°C dengan interval 100°C menggunakan mesin SCHENK TREBEL Machine. Hasil yang didapatkan pada penelitian ini, untuk gangguan mekanik pada nozzle case maksimum sebesar 7 MPa, beban mekanik ini sangat kecil jika dibandingkan dengan kekuatan tarik yang dimiliki komposit C/LY5052 dan C/ARMC, untuk beban termal pada Nozzle Case, pemanasan maksimum yang terjadi pada nozzle Case dengan rentang temperature 550ºC hingga 700°C, pada temperatur ini komposit C/LY5052 tidak bisa diterapkan karena hanya mampu bertahan sampai temperatur 200 ºC, hasil berbeda pada komposit C/ARMC pada saat rentang temperatur ini masih tangguh, maka dari hasil tersebut komposit C/ARMC dalam penelitian ini dapat dijadikan acuan sebagai alternatif material Nozzle Case. Namun ketika mendesain nozzle case dengan material komposit C/ARMC harus diperhatikan mode kegagalannya terutama mode kegagalan delaminasi.

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A rocket is a launch vehicle capable of transporting payload to the desired destination. The nozzle is the heaviest structural component, which contributes about 30% of the total weight of the rocket structure so it is very possible to reduce the weight. In designing the nozzle, one must also pay attention to the mechanical and thermal loads that are quite high due to the combustion of the propellant to produce rocket thrust. One alternative to reduce weight is the use of Carbon Fiber Reinforced Polymer Composite materials, to apply these composite materials to the nozzle case, it is necessary to characterize the mechanical properties. One of the most frequently performed tests is the tensile test. This test has a function to obtain values for strength, modulus of elasticity, and failure mode. Tensile testing is carried out in two stages to select materials that are capable of receiving thermal loads. The first stage of the tensile test was carried out with a temperature range from RT to 200°C using the Shimadzu AG-50KNX PLUS Machine for material selection between C/LY5052 and C/ARMC composites based on toughness at the temperature tested. Then the selected material is continued to the second stage of testing, where the selected material is tested in Tensile at a temperature range of RT to 800°C with intervals of 100°C using the SCHENK TREBEL Machine. The results obtained in this study, for maximum mechanical disturbance in the nozzle case of 7 MPa, this mechanical load is very small when compared to the tensile strength of the C/LY5052 and C/ARMC composites, for the thermal load on the Nozzle Case, the maximum heating that occurs on the Case nozzle with a temperature range of 550ºC to 700°C, at this temperature the C/LY5052 composite cannot be applied because it can only survive up to a temperature of 200 ºC, the results are different for the C/ARMC composite when this temperature range is still tough, so from these results, The C/ARMC composite in this study can be used as a reference as an alternative nozzle case material. However, when designing the nozzle case with C/ARMC composite material, the failure mode must be considered, especially the delamination failure mode."