• 제목/요약/키워드: forward surface

검색결과 444건 처리시간 0.019초

컴퓨터 작업시 책상과 체간사이 거리가 전방 머리 자세와 목과 어깨 근육들의 근 활성도에 미치는 영향 (Effect of Distance Between Trunk and Desk on Forward Head Posture and Muscle Activity of Neck and Shoulder Muscles During Computer Work)

  • 이원휘
    • 대한물리의학회지
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    • 제8권4호
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    • pp.601-608
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    • 2013
  • PURPOSE: The purpose of this study was to investigate the effect of distance between trunk and desk on forward head posture and muscle activity of neck and shoulder muscles during computer work. METHODS: Twenty subjects who have healthy conditions were asked to perform computer work in two conditions (distance between trunk and desk was 0 and 15 cm). Forward head angle was analyzed with a SIMI motion analysis system. Surface electromyography recorded the upper trapezius and splenius capitis muscles. The significance of differences in distance between trunk and desk (0cm and 15cm) was tested by paired t-test. The alpha level was set at .05. RESULTS: The results showed that the change of forward head angle was significantly higher during the computer work when the distance between trunk and desk was 15cm than 0cm. The muscle activity of upper trapezius and splenius capitis was also significantly higher during the computer work when the distance between trunk and desk was 15cm than 0cm. CONCLUSION: Our study suggest that the distance between trunk and desk was should minimized for prevention of forward head posture during computer work.

전방압출 공정에서 제품 변형 이력 (Deformation History of Product during Forward Extrusion Process)

  • 박용복
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 1999년도 춘계학술대회논문집
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    • pp.76-79
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    • 1999
  • The study has been performed for the relation between die and product in forward extrusion by the experiment. Strains of the die have been given by the simple experiment using the strain gauge located at the outer surface of the die and the history of the deformation of the die and product is given by the experiment and Lame's formula. The inner pressure of the die causes the deformation of die that affects the accuracy of dimension and shape of product. The product with accurate dimension and shape can be obtained by analysing elastic deformation of the die during process. The deformation of the die during metal forming process has been usually predicted by the experience of industrial engineer or finite element analysis. But it is difficult to predict the dimension of product at unloading and ejected states. The study has given useful results for the deformation history of the die and product through the experiment and Lame's formula at forward extrusion for solid cylinder and can be applied to the die design for product with accurate dimension.

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Solution of the Radiation Problem by the B-Spline Higher Order Kelvin Panel Method for an Oscillating Cylinder Advancing in the Free Surface

  • Hong, Do-Chun;Lee, Chang-Sup
    • Journal of Ship and Ocean Technology
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    • 제6권1호
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    • pp.34-53
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    • 2002
  • Numerical solution of the forward-speed radiation problem for a half-immersed cylinder advancing in regular waves is presented by making use of the improved Green integral equation in the frequency domain. The B-spline higher order panel method is employed stance the potential and its derivative are unknown at the same time. The present numerical solution of the improved Green integral equation by the B-spline higher order Kelvin panel method is shown to be free of irregular frequencies which are present in the Green integral equation using the forward-speed Kelvin-type Green function.

전진익형 항공기 공력특성 증진을 위한 풍동시험 (Wind Tunnel Test to Enhance Aerodynamic Characteristics of Forward Swept Wing Airplane)

  • 정진덕;이장연;성봉주;이종원
    • 대한기계학회논문집B
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    • 제28권7호
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    • pp.800-808
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    • 2004
  • Wind tunnel test of an airplane model with forward swept wing was done in KARI LSWT to evaluate and measure the aerodynamic characteristics of initially designed configuration. Since the given wing planform did not fully satisfy the design requirements, local flow control devices such as vortilon, vortex generator and flow fence were used to delay separation and to enhance aerodynamic characteristics. Also decision making processes of design parameters such as vertical tail boom length, the location, size and the incidence angle of horizontal tail were discussed. The general aerodynamic characteristics of forward swept wing for various control surface deflection conditions of flap, aileron and elevator were also given.

전방압출 공정에서 제품 변형 이력 (Deformation History of Product during Forward Extrusion Process)

  • 이강희;박용복
    • 소성∙가공
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    • 제10권1호
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    • pp.75-79
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    • 2001
  • The study has been performed for the relation between die and product during forward extrusion by the experiment. Stains of the die have been given by the simple experiment using the strain gauge located at the outer surface of the die. The history of the deformation of the die and the product has been given by the experiment and Lame's formula. The inner pressure of the die causes the deformation of die that affects the accuracy of dimension as well as shape of the product. The product with accurate dimension and shape can be obtained by analysing elastic deformation of the die during the process. The deformation of the die during metal forming process has been usually predicted by the experience of industrial engineer or finite element analysis. But it is difficult to predict the dimension of the product at unloading and ejected states. In the present study, useful results for the deformation history of the die and the product were obtained through the experiment and Lame's formula in forward extrusion which can be applied to the die design for the product with accurate dimension.

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CAE Solid Element Mesh Generation from 3D Laser Scanned Surface Point Coordinates

  • Jarng S.S.;Yang H.J.;Lee J.H.
    • 한국CDE학회논문집
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    • 제10권3호
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    • pp.162-167
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    • 2005
  • A 3D solid element mesh generation algorithm was newly developed. 3D surface points of global rectangular coordinates were supplied by a 3D laser scanner. The algorithm is strait forward and simple but it generates hexahedral solid elements. Then, the surface rectangular elements were generated from the solid elements. The key of the algorithm is elimination of unnecessary elements and 3D boundary surface fitting using given 3D surface point data.

RCS Numerical Simulation of Stealth Modified Three-Surface Aircraft

  • Cheng, Liangliang;Yue, Kuizhi;Xing, CuiFang;Yu, Dazhao
    • International Journal of Aeronautical and Space Sciences
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    • 제17권1호
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    • pp.101-108
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    • 2016
  • The RCS characteristics of stealth modified three-surface aircraft are analyzed in this paper. Prototype A is built with CATIA software and the three-dimensional digital models of modified stealth three-surface B and C are also designed based on carrier-based aircraft Su-33; the numerical simulation of RCS characteristics of three-surface aircraft is conducted with RCSAnsys software based on physical optics method and the method of equivalent currents; The following results are obtained by comparative analysis and mathematical statistics: (1) by the use of physical optics method and equivalent electromagnetic current method, the scattering intensity for each part of the model and RCS characteristic of the aircraft can be analyzed efficiently and accurately; (2) compared with model A, the mean RCS value of model B is reduced to 14.1% in forward direction and 48.1% in lateral direction; (3) compared with model A, the mean RCS value of model C decreases to 11.4% in forward direction and 21.6% in lateral direction. The results are expected to provide theoretical basis and technical support to the conceptual design of aircraft and stealth technology research.

전진 동요하는 잠수구에 의한 비선형 조파문제의 시간영역 해석 (Time Domain Analysis of Nonlinear Wave-Making Problems by a Submerged Sphere Oscillating with Forward Speed)

  • 하영록;배성용
    • 동력기계공학회지
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    • 제14권6호
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    • pp.75-82
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    • 2010
  • In this study, the topics for free-surface wave simulation, nonlinear hydrodynamic force, and the critical resonance frequency of so-called ${\tau}=U{\omega}/g$=1/4 are discussed. A high-order spectral/boundary element method is newly adapted as an efficient numerical tool. This method is one of the most efficient numerical methods by which the nonlinear gravity waves can be simulated and hydrodynamic forces also can be calculated in time domain. In this method, the velocity potential is expressed as the sum of surface potential and body potential. Then, surface potential is solved by using the high-order spectral method and body potential is solved by using the high-order boundary element method. By the combination of these two methods, the wave-making problems by a submerged sphere oscillating with forward speed under the free-surface are solved in time domain.

흉부 X-선 검사에서 복부비만에 따른 입사표면선량과 영상 왜곡도 평가 (Assessment of Entrance Surface Dose and Image Distortion in Accordance with Abdominal Obesity in the Chest Radiography)

  • 김부순;박정규;권순무
    • 한국방사선학회논문지
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    • 제9권7호
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    • pp.473-478
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    • 2015
  • 사회 인구학적 특성을 보정 하였을 때 대사 증후군의 예측에 가장 높은 연관이 남녀 모두에서 비만-복부 비만군이라고 보고되고 있으며, 의료기기의 발전과 더불어 방사선에 대한 피폭선량이 증가하고 있는 추세이다. 이에 흉부 X선 검사에서 복부의 비만정도를 가정하여 흉부팬텀에서 앞쪽방향(forward)으로 각도를 부여한 후 기준영상과 비교하여 입사표면선량과 영상의 왜곡 정도를 평가하였다. 흉부팬텀의 각도가 앞쪽방향으로 $5^{\circ}$ 증가할 때 마다 폐의 가로직경은 1.22%, 세로직경은 0.44% 증가하였다. 심장직경은 앞쪽방향으로 $5^{\circ}$ 증가할 때 마다 1.01% 증가, CTR은 0.27% 감소가 관찰되었다. 그 중 폐의 가로직경이 가장 큰 증가, 폐의 세로직경이 가장 작은 증가를 보였고 CTR은 작은 감소를 보였다. 그러나 팬텀에 입사하는 표면선량 측정의 경우, 흉부팬텀의 각도가 앞쪽방향으로 $5^{\circ}$ 증가할 때 마다 6.12%의 비교적 큰 증가를 보였다. 임상에서 흉부 X-선 후전방향촬영을 시행하는 경우, 복부비만 등으로 인해 흉부의 각도가 기울어짐에 따라 영상의 왜곡뿐만 아니라 환자에게 노출되는 선량이 증가되고 재촬영으로 추가적인 방사선 피폭이 발생될 수 있으므로 올바른 위치잡이에 주의를 기울여 환자의 방사선피폭 감소에 노력을 해야 할 것이다.

두경부(Head & Neck)종양에서 Forward IMRT 유용성에 관한 고찰 (The usefulness of Forward IMRT for Head and Neck Cancer)

  • 백금문;김대섭;박광호;김정만
    • 대한방사선치료학회지
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    • 제15권1호
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    • pp.41-52
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    • 2003
  • I. 목적 방사선 치료계획에 있어서 정상조직의 선량과 치료부위 선량의 분포는 매우 중요하다. 또한 치료부위의 균일한 선량분포를 얻기 위하여 여러 가지 방법을 이용하고 있다. 특히 두경부(Head & Neck) 종양의 방사선 치료 시 체표 윤곽의 변화가 심하여 이에 따른 선량 불균일 보정이 필요하다. 기존의 치료방법으로는 parotid gland 와 spinal cord 의 tolerance dose 이하를 유지하면서 planning target volume(PTV)에 충분한 치료 선량을 전달하기에는 여러 가지 어려움이 있다. 이에 본원에서는 Forward IMRT를 이용한 방사선 치료의 유용성 및 실용적인 정도관리 방법에 관한 연구를 하였다. II. 대상 및 방법 본 연구는 두경부(Head & Neck) 종양 비인두암(nasophrygeal cancer)의 방사선 치료가 요구되는 환자를 대상으로 하여 2차원적인 치료계획과 dynamic Mulit-Leaf Collimator(dMLC)를 이용하여 partial block technique(PBT)방법을 적용한 Forward IMRT를 위한 치료계획을 dose volume histogram(DVH)로 비교 분석하였다. 또한 정도관리(quality assurance, QA)를 위하여 필름과 pinpoint chamber를 이용하여 정확한 선량 평가를 실시하였다. III. 결과 2차원적인 치료계획과 Forward IMRT를 적용한 치료계획의 DVH를 비교 분석한 결과 Forward IMRT를 적용한 치료계획이 Rt, Lt parotid gland와 spinal cord에 들어가는 선량을 좀더 줄일 수 있었다. 이러한 Forward IMRT의 시도로 조사면의 방사선 세기가 정상조직의 보호를 개선시키고 치료의 최적화를 이룰 수 있었다. Inverse IMRT에 비해 기존의 3차원적 치료계획 장치를 이용할 수 있고 비교적 단순한 방사선 세기 패턴이므로 정도관리가 용이하였다. IV. 결론 Forward IMRT는 2차원적인 치료법에 비하여 PTV에는 균일한 선량분포를 이루면서 정상조직에는 tolerance dose 이하로 선량을 전달 할 수 있는 치료기법이었다.

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