• 제목/요약/키워드: heat coefficient

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전방향족 공중합체의 열경화성 액정필름 (Liquid Crystalline Thermoset Films Based on Wholly Aromatic Copolymers)

  • 문현곤;안용호;장진해
    • 폴리머
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    • 제34권4호
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    • pp.369-375
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    • 2010
  • 용융 중합법을 이용하여 말단에 메틸 말레이미드(methyl maleimide) 반응성기를 가지며 방향족 에스터와 아 미드 결합을 포함하는 액정(liquid crystal, LC)을 합성하였다. 합성된 액정은 용액 캐스팅과 열처리를 거쳐 열경화 성 액정(liquid crystalline thermoset, LCT) 필름으로 제조되었다. 합성된 LC 및 LCT는 적외선 분광기(FTIR), 시차주사 열량계(DSC), 열중량 분석기(TGA), 열-기계 분석기(TMA), X-선 회절기(XRD) 및 가열판이 부착된 편광 현미경(POM) 등을 이용해서 각각 특성 분석을 하였다. 합성된 모든 액정은 스멕틱(smectic) 상을 보였으며 LC와 LCT들의 열적 성질은 주로 주사슬에 포함된 메소젠 구조에 영향을 받았다. 열팽창 계수(coefficients of thermal expansion, CTE)는 27.72~50.95 ppm/$^{\circ}C$ 사이의 값을 보였다.

수소 저장용 탱크의 튜브 형상에 따른 온도분포 특성에 대한 수치해석 연구 (A Study on the Characteristics of Temperature Distribution Related to Geometry of Tube in Hydrogen Storage Vessel)

  • 오승준;윤정환;전경숙;김재규;박준홍;최정주
    • 한국수소및신에너지학회논문집
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    • 제32권4호
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    • pp.205-211
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    • 2021
  • Recently, it is necessary for study on renewable energy due to environmental pollution and fossil fuel depletion. Therefore, in this study, the filling temperature according to the nozzle geometry was evaluated based on the limit temperature specified in SAEJ2601 for charging hydrogen, a new energy. There are three types of nozzles, normal, angle and round, fixed the average pressure ramp rate at 52.5 MPa/min, and the injection temperature was set at 293.4 K. As a result, the lowest temperature distribution was found in the round type, although the final temperature did not differ significantly in the three types of nozzles. In addition, Pearson's coefficient was calculated to correlate the mass flow rate with the heat transfer rate at the inner liner wall, which resulted in a strong linear relationship of 0.98 or higher.

고도 변화에 따른 전투기 적외선 신호 최소 조건 분석 (Effect of Flight Altitude on Minimal Infrared Signature of Combat Aircraft)

  • 남주영;장인중;이용우;김지현;조형희
    • 한국전산구조공학회논문집
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    • 제33권6호
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    • pp.375-382
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    • 2020
  • 적외선 유도 무기 체계의 발달로 항공기의 생존성은 지속적으로 위협받고 있으며, 항공기의 생존성을 향상시키기 위한 적외선 스텔스 기술 관련 연구가 진행되고 있다. 본 논문에서는 적외선 유도 미사일이 항공기와 배경 간의 대비 신호를 탐지하는 것에 주목하여 비행 조건에 따른 항공기의 최적 적외선 신호를 분석하고자 하였다. 이를 위해 항공기의 비행 조건을 고려하여 유동 해석과 대류, 전도, 복사 3차원 열전달 해석을 수행하였고, 동체 표면 온도를 도출하여 항공기 주변 유동 특성을 기반으로 항공기의 적외선 신호를 분석하였다. 더 나아가, 비행 조건 별로 최적 적외선 신호를 갖기 위한 최적 방사율을 도출하였고, 비행 조건 별로 최적 방사율을 동체 표면에 적용했을 때 적외선 신호 저감 효과를 분석하였다.

압력용기로부터 압력방출장치를 통한 가스 방출에 관한 포괄적 고찰 (Comprehensive Consideration on the Discharge of Gases from Pressurized Vessels through Pressure Relief Devices)

  • 정창복
    • 한국안전학회지
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    • 제35권6호
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    • pp.32-45
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    • 2020
  • The problem of determining the discharge rates of gases from pressurized vessels through pressure relief devices was dealt with comprehensively. First, starting from basic fluid flow equations, detailed modeling procedures were presented for isentropic nozzle flows and frictional flows in a pipe, respectively. Meanwhile, physical explanations were given to choking phenomena in terms of the acoustic velocity, elucidating the widespread use of Mach numbers in gas flow models. Frictional flows in a pipe were classified into adiabatic, isothermal, and general flows according to the heat transfer situation around the pipe, but the adiabatic flow model was recommended suitable for gas discharge through pressure relief devices. Next, for the isentropic nozzle flow followed by adiabatic frictional flow in the pipe, two equations were established for two unknowns that consist of the Mach numbers at the inlet and outlet of the pipe, respectively. The relationship among the ratio of downstream reservoir pressure to upstream pressure, mass flux, and total frictional loss coefficient was shown in various forms of MATLAB 2-D plot, 3-D surface plot and contour plot. Then, the profiles of gas properties and velocity in the pipe section were traced. A method to quantify the relationship among the pressure head, velocity head, and total friction loss was presented, and was used in inferring that the rapid increase in gas velocity in the region approaching the choked flow at the pipe outlet is attributed to the conversion of internal energy to kinetic energy. Finally, the Levenspiel chart reproduced in this work was compared with the Lapple chart used in API 521 Standatd.

중적외선 센서 위성 영상의 상온 온도 정보 추출 가능성 및 정확도 (Possibility and Accuracy of Extracting Room Temperature Information from Mid-Infrared Sensor Satellite Images)

  • 최석원;서두천;이동한
    • 우주기술과 응용
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    • 제1권3호
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    • pp.356-363
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    • 2021
  • 중적외선을 이용하여 획득한 영상은 상온 부근의 온도 측정에는 적당하지 않다는 것이 교과서적 상식이었으나, 최근 중적외선 센서를 이용한 위성 영상을 살펴보면 중적외선 센서를 이용하여 측정한 결과물도 상온 부근의 온도를 측정할 수 있다는 가능성을 보여주고 있다. 본 논문에서는 중적외선 센서를 가지는 위성영상의 상온 온도 정보 추출 가능성 및 정확도에 대해 살펴보고자 한다. 논문에서 검토된 중적외선 위성영상은 상온 부분의 온도를 잘 표시하였으며, 측정된 온도의 절대값으로서의 신뢰성에 관해서는, 태양광의 지표면 직접 반사에 의한 열전달량 영향과 대기에서 흡수되는 적외선 대기 흡수량의 영향은 비교적 작거나 일정한 값으로 볼 수 있지만, 비접촉식 온도계의 한계인 물성치의 의한 복사 계수(emissivity)의 불확실성 문제는 여전히 해결해야할 문제로 남아 있게 되었다.

저융점 Sn-Bi 솔더의 신뢰성 개선 연구 (Improvement of Reliability of Low-melting Temperature Sn-Bi Solder)

  • 정민성;김현태;윤정원
    • 마이크로전자및패키징학회지
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    • 제29권2호
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    • pp.1-10
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    • 2022
  • 최근 반도체 소자는 모바일 전자제품과 wearable 및 flexible한 소자와 기판의 다양한 활용으로 많은 분야에서 폭넓게 사용되고 있다. 이들 반도체 칩 접합 공정 중 기판과 솔더의 열팽창 계수(CTE)의 차이와 기판 및 부품 전체에 인가되는 과도한 열 영향은 소자의 성능 및 신뢰성에 영향을 주며, 최종적으로 휨(warpage) 현상 및 장기 신뢰성 저하 등을 초래한다. 이러한 문제점을 개선하기 위해 저온에서 공정이 가능한 저융점 솔더에 대한 연구가 활발히 진행되고 있다. Sn-Bi, Sn-In 등 다양한 저융점 솔더 합금 중 Sn-Bi 솔더는 높은 항복 강도, 적절한 기계적 특성 및 저렴한 가격 등의 이점이 있어 유망한 저온 솔더로 각광받고 있다. 그러나 Bi의 높은 취성 특성 등 단점으로 인해 솔더 합금의 개선이 필요하다. 본 review 논문에서는 다양한 미량 원소와 입자를 첨가하여 Sn-Bi 소재의 기계적 특성 개선을 위한 연구 동향을 소개하며 이를 비교 분석하였다.

다결정 산화갈륨/다이아몬드 이종 박막 성장 및 열처리 효과 연구 (Growth and thermal annealing of polycrystalline Ga2O3/diamond thin films on Si substrates)

  • 서지연;김태규;신윤지;정성민;배시영
    • 한국결정성장학회지
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    • 제31권6호
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    • pp.233-239
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    • 2021
  • 본 연구에서는 산화갈륨의 방열 특성 향상을 위해 산화갈륨/다이아몬드 이종 박막 성장을 진행하였다. 먼저, 핫필라멘트 화학기상증착법을 이용하여 다결정 다이아몬드를 증착시킨 후, 미스트 화학기상증착법을 통해 450~600℃ 사이의 온도구간에서 산화갈륨 박막을 성장시켰다. 열처리 전후 비교를 통해 500℃에서 산화갈륨/다이아몬드 계면 분리 현상이 발생함을 확인하였다. 이는 비정질과 결정질이 혼재된 산화갈륨 박막이 성장된 후, 냉각 과정에서 열팽창계수의 차이로 인해 계면이 분리된 것으로 판단하였다. 따라서, 본 연구를 통한 산화갈륨/다이아몬드 계면의 물리적 안정성을 통해 산화갈륨의 열물성 보완및 고전력 반도체로의 활용이 기대된다.

Experimental and numerical FEM of woven GFRP composites during drilling

  • Abd-Elwahed, Mohamed S.;Khashaba, Usama A.;Ahmed, Khaled I.;Eltaher, Mohamed A.;Najjar, Ismael;Melaibari, Ammar;Abdraboh, Azza M.
    • Structural Engineering and Mechanics
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    • 제80권5호
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    • pp.503-522
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    • 2021
  • This paper investigates experimentally and numerically the influence of drilling process on the mechanical and thermomechanical behaviors of woven glass fiber reinforced polymer (GFRP) composite plate. Through the experimental analysis, a CNC machine with cemented carbide drill (point angles 𝜙=118° and 6 mm diameter) was used to drill a woven GFRP laminated squared plate with a length of 36.6 mm and different thicknesses. A produced temperature during drilling "heat affected zone (HAZ)" was measured by two different procedures using thermal IR camera and thermocouples. A thrust force and cutting torque were measured by a Kistler 9272 dynamometer. The delamination factors were evaluated by the image processing technique. Finite element model (FEM) has been developed by using LS-Dyna to simulate the drilling processing and validate the thrust force and torque with those obtained by experimental technique. It is found that, the present finite element model has the capability to predict the force and torque efficiently at various drilling conditions. Numerical parametric analysis is presented to illustrate the influences of the speeding up, coefficient of friction, element type, and mass scaling effects on the calculated thrust force, torque and calculation's cost. It is found that, the cutting time can be adjusted by drilling parameters (feed, speed, and specimen thickness) to control the induced temperature and thus, the force, torque and delamination factor in drilling GFRP composites. The delamination of woven GFRP is accompanied with edge chipping, spalling, and uncut fibers.

Two-dimensional curved panel vibration and flutter analysis in the frequency and time domain under thermal and in-plane load

  • Moosazadeh, Hamid;Mohammadi, Mohammad M.
    • Advances in aircraft and spacecraft science
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    • 제8권4호
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    • pp.345-372
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    • 2021
  • The analysis of nonlinear vibrations, buckling, post-buckling, flutter boundary determination and post-flutter behavior of a homogeneous curved plate assuming cylindrical bending is conducted in this article. Other assumptions include simply-supported boundary conditions, supersonic aerodynamic flow at the top of the plate, constant pressure conditions below the plate, non-viscous flow model (using first- and third-order piston theory), nonlinear structural model with large deformations, and application of mechanical and thermal loads on the curved plate. The analysis is performed with constant environmental indicators (flow density, heat, Reynolds number and Mach number). The material properties (i.e., coefficient of thermal expansion and modulus of elasticity) are temperature-dependent. The equations are derived using the principle of virtual displacement. Furthermore, based on the definitions of virtual work, the potential and kinetic energy of the final relations in the integral form, and the governing nonlinear differential equations are obtained after fractional integration. This problem is solved using two approaches. The frequency analysis and flutter are studied in the first approach by transferring the handle of ordinary differential equations to the state space, calculating the system Jacobin matrix and analyzing the eigenvalue to determine the instability conditions. The second approach discusses the nonlinear frequency analysis and nonlinear flutter using the semi-analytical solution of governing differential equations based on the weighted residual method. The partial differential equations are converted to ordinary differential equations, after which they are solved based on the Runge-Kutta fourth- and fifth-order methods. The comparison between the results of frequency and flutter analysis of curved plate is linearly and nonlinearly performed for the first time. The results show that the plate curvature has a profound impact on the instability boundary of the plate under supersonic aerodynamic loading. The flutter boundary decreases with growing thermal load and increases with growing curvature.

An effective automated ontology construction based on the agriculture domain

  • Deepa, Rajendran;Vigneshwari, Srinivasan
    • ETRI Journal
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    • 제44권4호
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    • pp.573-587
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    • 2022
  • The agricultural sector is completely different from other sectors since it completely relies on various natural and climatic factors. Climate changes have many effects, including lack of annual rainfall and pests, heat waves, changes in sea level, and global ozone/atmospheric CO2 fluctuation, on land and agriculture in similar ways. Climate change also affects the environment. Based on these factors, farmers chose their crops to increase productivity in their fields. Many existing agricultural ontologies are either domain-specific or have been created with minimal vocabulary and no proper evaluation framework has been implemented. A new agricultural ontology focused on subdomains is designed to assist farmers using Jaccard relative extractor (JRE) and Naïve Bayes algorithm. The JRE is used to find the similarity between two sentences and words in the agricultural documents and the relationship between two terms is identified via the Naïve Bayes algorithm. In the proposed method, the preprocessing of data is carried out through natural language processing techniques and the tags whose dimensions are reduced are subjected to rule-based formal concept analysis and mapping. The subdomain ontologies of weather, pest, and soil are built separately, and the overall agricultural ontology are built around them. The gold standard for the lexical layer is used to evaluate the proposed technique, and its performance is analyzed by comparing it with different state-of-the-art systems. Precision, recall, F-measure, Matthews correlation coefficient, receiver operating characteristic curve area, and precision-recall curve area are the performance metrics used to analyze the performance. The proposed methodology gives a precision score of 94.40% when compared with the decision tree(83.94%) and K-nearest neighbor algorithm(86.89%) for agricultural ontology construction.