• Title/Summary/Keyword: honeycomb structure

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Design and Fabrication of X-band Wideband Array Antenna for SAR Applications (SAR를 위한 X-band 광대역 배열 안테나의 설계 및 제작)

  • Won Young-Jin;Lee Young-Ju;Kong Young-Kyun
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.17 no.2 s.105
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    • pp.184-192
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    • 2006
  • Synthetic Aperture Radars(SAR) are used mainly for high-resolution imaging of the terrain. This paper describes the $16{\times}16$ array antenna designed for an X-band, automobile-based SAR(AutoSAR) system. This antenna has the structure of several layers such as radome, radiators, slots, feed network, and honeycomb cores. Each layer is adhesively bonded to meet different combination of structural and electrical design requirements. Using the Strip-Slot-Foam-Inverted-Patch(SSFIP) structure and honeycomb cores, a wide bandwidth and a structural hardness were achieved. Measurement results were compared with simulation results. It was observed that this antenna had a bandwidth of 1.7 GHz, side-lobe levels of less than -20 dB, half-power beamwidth of $5^{\circ}$ and $5^{\circ}$, and gains of 25.0 dBi. The observed results show that the designed array antenna will be applicable to the wideband SAR system.

Design and implementation of the honeycomb structure visualization system for the effective security situational awareness of large-scale networks (대규모 네트워크의 효과적 보안상황 인지를 위한 벌집 구조 시각화 시스템의 설계 및 구현)

  • Park, Jae-Beom;Kim, Huy-Kang;Kim, Eun-Jin
    • Journal of the Korea Institute of Information Security & Cryptology
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    • v.24 no.6
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    • pp.1197-1213
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    • 2014
  • Due to the increase in size of the computer network, the network security systems such as a firewall, IDS, IPS generate much more vast amount of information related to network security. So detecting signs of hidden security threats has become more difficult. Security personnels' 'Network Security Situational Awareness(NSSA)' is effectively determining the security situation of overall computer network on the basis of the relation between the security events that occur in the several views. The process of situational awareness is divided into three stages of the 'identification,' 'understanding' and 'prediction'. And 'identification' and 'understanding' are prerequisites for 'predicting' and the following appropriate responses. But 'identification' and 'understanding' in the vast amount of information became more difficult. In this paper, we propose Honeycomb security situational awareness visualization system that is designed to help NSSA in large-scale networks by using visualization techniques known effective to the 'identification' and 'understanding' stages. And we identified the empirical effects of this system on the basis of the 'VAST Challenge 2012' data.

Detection of Real Defects in Composite Structures by Using Laser Measuring System (레이저 계측시스템을 이용한 복합재료 구조물의 실제결함 검출)

  • 김태형;정성균;김경석;장호섭
    • Proceedings of the Korean Society For Composite Materials Conference
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    • 2002.05a
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    • pp.35-38
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    • 2002
  • Real defects in composite structures were detected by using laser measuring system. Four types of specimens, that is, a composite laminate, a honeycomb structure, a free-edge delamination and an adhesive joint, were used to study the applicability of ESPI and Shearography to composite structures. Thermal loading method, which can easily induce the surface deformation of specimen, was used to detect defects. Experimental results show that defects in composite structures can be easily detected by ESPI and Shearography. Moreover, it shows that ESPI and Shearography can be usefully applied to the detection of defects in various kinds of composite structures.

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A study on Development of Stress Tolerant Structural System in the Frame of Greenhouses (내재해성이 우수한 비닐하우스골조 구조시스템 개발에 관한 연구)

  • Shim, Jong-Seok;Lee, Choon-Ho
    • Journal of The Korean Digital Architecture Interior Association
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    • v.12 no.1
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    • pp.5-13
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    • 2012
  • The frame of pipe greenhouses in Korea have been collapsed increasingly due to very weak in structure caused by the heavy snow and strong wind. In order to reduce the collapse of green houses, it is urgent to develop the new structural system in stress tolerant greenhouses. Therefore, this paper performed the structural analysis of greenhouse frame in accordance with snow loads and wind loads. Three type models in structural frame configuration of greenhouses, that is, existing type, diagrid type, and honeycomb type are selected. It was classfied the section shape of structural frames in greenhouses into arch style, standard style, and diagonal standard style. As a result of this paper, it was verified that the structural system of diagrid type is better than that of existing type against snow loads and wind loads in the frame of greenhouses.

Design, Fabrication and Test of Smart Skin Sandwich Specimen (스마트 스킨 샌드위치 시편의 설계, 제작 및 시험 평가)

  • 김용범;김영성;박훈철;윤광준;이재화
    • Composites Research
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    • v.15 no.3
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    • pp.45-51
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    • 2002
  • Smart skin, a multi-layer structure of composed or different materials, was designed and fabricated. Tests and analyses are conducted to study the characteristics of its behavior under compression and bending loads. The designed smart skin failed due to premature buckling before compression failure. It was confirmed that shear moduli of honeycomb core affect structural stability of smart skin. A new test method and device were designed fur better measurement of shear moduli of honeycomb core. Numerical prediction of structural behavior of smart skin by NASTRAN agreed well with experimental data.

Evaluation of the Physical and the Mechanical Properties of the High Frictional Resistance Prepreg and the Low Frictional Resistance Prepreg (고마찰저항 프리프레그와 저마찰저항 프리프레그의 물리적 및 기계적 특성평가)

  • Kim, Y.H.;Han, J.W.;Kim, K.J.;Kim, J.H.;Son, J.H.
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.06a
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    • pp.326-330
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    • 2005
  • Aircraft composite structure with honeycomb core experiences core crush problem in manufacturing. To prevent core crush additional processes are needed such as core stabilization and prepreg material tie-down and this is the cause of increasing cost. Recent study shows that high friction prepreg prevent core crush without additional process. This paper presents the analysis of high frictional material which attracts lots of interests through physical property, mechanical property and microscopic

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An Evaluation of Structural Strength by Testing the Carbody of Light Composite Material (경량 복합소재 차체의 시험에 의한 구조강도 평가)

  • Yoon S.C.;Jeon C.S.;Kim W.K.;Kim M.Y.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2006.05a
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    • pp.393-394
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    • 2006
  • This study introduces the testing results of the composite carbody which is applied to tilting train. The composite carbody is made of aluminum honeycomb structure materials like a sandwich. The static load test was performed to evaluate the structural characteristic and stability of the composite carbody. Considering the vertical, compressive, twisting load and 3-point supporting type as a testing terms, the structural stability of a carbody was evaluated.

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Prediction of the Mechanical Properties of the Nano-sized Honeycomb Structures with Surface Effects (표면 효과가 있는 나노 허니콤 구조의 기계적 물성의 예측)

  • Lee, Yong-Hee;Jeong, Joon-Ho;Cho, Maeng-Hyo
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2011.04a
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    • pp.261-264
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    • 2011
  • 유한 요소 기법을 이용한 허니콤 구조물의 해석은 모델링 작업 및 격자 생성의 어려움뿐만 아니라 과도한 해석 시간이 요구되기 때문에 균질화 기법은 계산상의 효율성을 증대시킬 수 있는 매우 유용한 방법이라 할 수 있다. 그러나 나노 크기의 구조물에서는 표면 효과로 인하여 거시적인 구조물에서와는 매우 상이한 기계적 거동 양상을 띠게 되며 균질화 기법을 나노 크기의 허니콤 구조물에 적용하기 위해서는 이러한 표면 효과를 반영해야만 한다. 본 논문에서는 표면 효과를 고려한 유한 요소를 제안하고 이를 이용하여 나노 크기의 3차원 허니콤 구조물을 균질화 기법을 이용하여 등가의 2차원 판으로 대체하였다.

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The characteristic evaluation of high frictional resistance prepreg influencing honeycomb core crush (하니컴 코어 붕괴에 영향을 주는 고 마찰 저항 프리프레그의 특성 평가)

  • Han J. W.;Kim G. J.;Kim J. M.;Jin Y. J.;Seo J. J.;Kim J. H.
    • Proceedings of the Korean Society For Composite Materials Conference
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    • 2004.04a
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    • pp.270-274
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    • 2004
  • Aircraft composite structure with honeycomb core experiences core crush problem in manufacturing. To prevent core crush additional processes are needed such as core stabilization and prepreg material tie-down and this is the cause of increasing cost. Recent study shows that high friction prepreg prevent core crush without additional process. This paper presents the analysis of high frictional material which attracts lots of interests through physical property, mechanical property and microscopic morphology and the cause of friction.

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UPHILL ZAGREB INDICES OF SOME GRAPH OPERATIONS FOR CERTAIN GRAPHS

  • SALEH, ANWAR;BAZHEAR, SARA;MUTHANA, NAJAT
    • Journal of applied mathematics & informatics
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    • v.40 no.5_6
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    • pp.959-977
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    • 2022
  • The topological indices are numerical parameters which determined the biological, physical and chemical properties based on the structure of the chemical compounds. One of the recently topological indices is the uphill Zagreb indices. In this paper, the formulae of some uphill Zagreb indices for a few graph operations of some graphs have been derived. Furthermore, the precise formulae of those indices for the honeycomb network have been found along with their graphical profiles.