• 한국강구조학회 논문집
• /
• 제26권6호
• /
• pp.499-509
• /
• 2014

본 연구에서는 해결방안으로 내부 콘크리트를 강섬유와 혼입하여 기둥자체의 연성과 인성을 증대시키는 것에 중점을 맞추고 있다. 즉, 강섬유 혼입량과 하중조건에 따른 내력 및 변형능력을 종합적으로 파악하여 강섬유 콘크리트와 용접조립각형 강관기둥의 상호작용을 구조, 내화측면에서 분석해 보고자 한다. 동일한 형상과 경계조건(하중비)에서 강섬유 혼입(0.375%)으로 내화성능은 약 1.1~1.3배 향상된 실험결과를 얻을 수 있었다. 강섬유 콘크리트의 균열 억제 특성은 열 하중에 의한 콘크리트의 변형저항 성능을 증가 시키면서 내화성능의 향상을 가져온 것으로 판단된다. 또한, 내부 리브의 열 변형에도 내부 콘크리트 단면은 건전한 상태로 남아있어 하중 분담능력이 증폭된 결과로 분석됐다.

• 한국염색가공학회지
• /
• 제32권4호
• /
• pp.274-280
• /
• 2020

This study compared the mechanical properties of bamboo fiber composites and kenaf fiber composites through physical treatment (ultrasonic treatment). Kenaf, a composite of PP reinforced with bamboo fiber, was made using injection molding technology. PP was used as a binder and the ultrasonic treatment time of bamboo and kenaf was increased by 30 minutes to compare and study various mechanical properties of bamboo and kenaf composites through physical treatment. Interfacial properties such as internal cracks and internal structure of the wave cross section were confirmed using a scanning electron microscope (SEM). As a result of the ultrasonic treatment, most of the characteristics were fragile as the ultrasonic treatment time was increased, and it was confirmed that the natural characteristics of the twisted fibers had a great influence on the characteristics of the composite material.

• 한국전산구조공학회논문집
• /
• 제30권3호
• /
• pp.255-263
• /
• 2017

본 논문에서는 합성단면을 갖는 구조물의 극한 거동 해석에서 요구하는 재료 및 기하학적 비선형 해석을 수행하기 위한 보 요소를 제시하였다. 제안된 요소는 기하학적 비선형성을 효과적으로 모사할 수 있는 co-rotational 정식화를 통해 도출되었으며, 다양한 합성단면의 저항성능을 재현할 수 있도록 화이버 단면법이 요소의 내력 및 강성을 산정하는데 활용되었다. 제안된 방법을 구현할 수 있도록 해석 프로그램이 개발되었으며, 호장법을 적용하여 최대내력 발생 이후의 연성거동뿐만 아니라 심한 비선형 응답(snap-through 또는 snapback)까지 추적해낼 수 있도록 하였다. 본 연구에서 제안된 요소 정식화와 해석 프로그램의 정확성을 검증을 위해 몇 가지 수치예제가 수행되었고, 해석결과는 제안된 요소의 정확성과 효율성을 보이기 위해 3차원 연속체 모델 및 기존 연구의 결과와 비교되었다. 추가로 합성단면을 갖는 골조 구조물에 대한 수치예제를 통해, 합성단면을 구성하는 재료의 탄성계수 비 및 강도 비에 따른 영향을 분석하였다. 해석결과는 외층 재료의 탄성계수가 증가됨에 따라 준취성 거동이 나타났으며, 외층 재료의 항복강도가 높을수록 선형 거동하는 기하적 비선형 응답과 유사한 응답을 보였다.

• Journal of the Korean Wood Science and Technology
• /
• 제44권3호
• /
• pp.295-301
• /
• 2016

본 연구는 4개 종자산지(Yugoslovia, ltaly, United Kingdom, Bulgaria)의 글로티노사오리나무(Alnus glutinosa)를 대상으로 목섬유 길이, 도관 길이 및 직경인 해부학적 성질을 조사하여, 이들의 종자산지 간 및 생장속도와의 관계를 규명하였다. 글로티노사오리나무는 산공재, 계단상천공, 교호상벽공으로 나타났다. 접선단면에서 방사조직 높이는 9~11, 횡단면에서 방사조직 수는 16~26개로 나타났다. 산지 간의 목섬유 길이, 도관 길이 및 직경에서 만재부에서는 차이가 없었고, 조재부에서는 차이가 있는 것으로 나타났다. 3개 산지는 생장이 좋을수록 만재부의 목섬유 및 도관 길이가 짧아지는 것으로 나타났으나, 유고슬로비아산은 생장이 좋으면서 목섬유 및 도관길이도 긴 것으로 나타났다.

• Computers and Concrete
• /
• 제11권2호
• /
• pp.105-121
• /
• 2013

This paper investigates the parameters that control the design of Fiber Reinforced Polymer (FRP) reinforced concrete flexural members proportioned following the ACI 440.1R-06. It investigates the critical parameters that control the flexural design, such as the deflection limits, crack limits, flexural capacity, concrete compressive strength, beam span and cross section, and bar diameter, at various Mean-Ambient Temperatures (MAT). The results of this research suggest that the deflection and cracking requirements are the two most controlling limits for FRP reinforced concrete flexural members.

• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 2003년도 봄 학술발표회 논문집
• /
• pp.561-566
• /
• 2003

In this study, to predict the behavior of RC beam strengthened with Carbon fiber reinforced polymer(CFRP) plate, analytical program considering material non-linearity is developed. Strain compatibility and force equilibrium are applied and internal forces of constitutive material are calculated using nonlinear stress-strain relationship. Also, to certainty the reliability of analytical program, deflection, strain of CFRP plate, change of neutral axis on cross section and crack distribution at failure are compared with those of experiment, and each results are almost coincident.

• Structural Engineering and Mechanics
• /
• 제37권6호
• /
• pp.649-669
• /
• 2011

In this paper an analytical model is presented that addresses the compressive response of short-fiber reinforced concrete members (FRC) with hooked steel fibers. This model is applicable to a wide range of concrete strengths and accounts for the interaction between the cover spalling and the concrete core confinement induced by transverse steel stirrups and also for buckling of longitudinal reinforcing bars. The load-shortening curves generated here analytically fit existing experimental data well.

• 한국생산제조학회지
• /
• 제21권4호
• /
• pp.619-624
• /
• 2012

In this study, MMT/fiber/polymer composites were fabricated by impregnating chopped strand glass mat into a vinylester resin mixed with clay. Tensile tests has been performed by using a universal testing machine to determine the effect of MMT addition on the tensile properties of MMT/chopped strand glass fiber/vinylester composites. And some pictures which are magnified cross section of breaking parts are has been taken by using a FE-SEM to confirm the behavior at breaking. The contents ratio of MMT applied in the composites were 0.5, 1.0, 1.5, and 2.0 wt% respectively. It has been found that the tensile strength and elastic modulus of MMT/chopped strand glass fiber/vinylester composites were improved at a proper content of MMT. Tensile strength and elastic modulus were maximized at a content of 1.0 wt% due to most effective dispersion of MMT. On the contrary, the failure strain was increased as MMT content was increased.

• Fibers and Polymers
• /
• 제3권4호
• /
• pp.129-133
• /
• 2002

It is well known residual gum exists in degummed or rotted hemp fibers. Gum removal results in improvement in fiber fineness and the properties of the resultant hemp yams. However, it is not known what correlation if any exists between the residual gum content in retted hemp fibers and the fiber fineness, described in terms of fiber width in this paper. This study examined the mean width and coefficient of variation (CV) of fiber width of seventeen chemically rotted hemp samples with reference to residual gum content. The mean and CV of fiber width were obtained from an Optical fiber diameter analyser (OFDA 100). The linear regression analysis results show that the mean fiber width is directly proportional to the residual gum content. A slightly weaker linear correlation also exists between the coefficient of variation of fiber width and the residual gum content. The strong linear co-relation between the mean of fiber width and the residual gum content is a significant outcome, since testing for fiber width using the OFDA is a much simpler and quicker process than testing the residual gum content. Scanning Electron Microscopy (SEM) reinforces the OFDA findings. SEM micrographs show a flat ribbon like fiber cross-section hence the term \"fiber width\" is used instead of fiber diameter. Spectral differences in the untreated dry decorticated skin samples and chemically treated and subsequently carded samples indicate delignification. The peaks at $1370cm^{-1}$, $1325cm^{-1}$, $1733cm^{-1}$, and $1600cm^{-1}$ attributed to lignin in the untreated samples are missing from the spectra of the treated samples. The spectra of the treated samples are more amine-dominated with some of the OH character lost.cter lost.

• International Journal of Aeronautical and Space Sciences
• /
• 제18권2호
• /
• pp.215-221
• /
• 2017

An electromagnetic (EM) wave absorber reduces the possibility of radar detection by minimizing the radar cross section (RCS) of structures. In this study, a radar absorbing structure (RAS) was applied to the leading edge of a blended wing body aircraft to reduce RCS in X-band (8.2~12.4GHz) radar. The RAS was composed of a periodic pattern resistive sheet with conductive lossy material and glass-fiber/epoxy composite as a spacer. The applied RAS is a multifunctional composite structure which has both electromagnetic (EM) wave absorbing ability and load-bearing ability. A two dimensional unit absorber was designed first in a flat-plate shape, and then the fabricated leading edge structure incorporating the above RAS was investigated, using simulated and free-space measured reflection loss data from the flat-plate absorber. The leading edge was implemented on the aircraft, and its RCS was measured with respect to various azimuth angles in both polarizations (VV and HH). The RCS reduction effect of the RAS was evaluated in comparison with a leading edge of carbon fabric reinforced plastics (CFRP). The designed leading edge structure was examined through static structural analysis for various aircraft load cases to check structural integrity in terms of margin of safety. The mechanical and structural characteristics of CFRP, RAS and CFRP with RAM structures were also discussed in terms of their weight.