• 제목/요약/키워드: Model Plane

검색결과 2,199건 처리시간 0.028초

반전력빔폭을 이용한 전방향성 안테나의 수중 환경 수직 평면 감쇠 모델 (Underwater E-plane Attenuation Model of Omnidirectional Antenna Using Half Power Beam Width (HPBW))

  • 곽경민;박대길;김영현;정완균;김진현
    • 제어로봇시스템학회논문지
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    • 제21권11호
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    • pp.1050-1056
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    • 2015
  • In this paper, we use the characteristics of electromagnetic waves underwater attenuation for estimating linear distance between a transmitting node and receiving node, and research underwater vertical plane attenuation model for constructing the underwater localization system. The underwater localization of 2 dimensional with the plane attenuation model in the horizontal plane (H-plane) was proposed previous research. But for the 3 dimensional underwater localization, the additional vertical plane (E-plane) model should be considered. Because the horizontal plane of omnidirectional antenna has the same attenuation tendency in x-y plane according to the distance, whereas in vertical plane shows an irregular pattern in x-z plane. For that reason, in the vertical plane environment, the attenuation should be changed by the position and inclination. Hence, in this paper the distance and angle between transmitting and receiving node are defined using spherical coordinate system and derive an antenna gain pattern using half power beam width (HPBW). The HPBW is called a term which defines antenna's performance between isotropic and other antennas. This paper derives omnidirectional antenna's maximum gain and attenuation pattern model and define vertical plane's gain pattern model using HPBW. Finally, experimental verifications for the proposed underwater vertical plane's attenuation model was executed.

Maneuvering simulation of an X-plane submarine using computational fluid dynamics

  • Cho, Yong Jae;Seok, Woochan;Cheon, Ki-Hyeon;Rhee, Shin Hyung
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제12권1호
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    • pp.843-855
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    • 2020
  • X-plane submarines show better maneuverability as they have much longer span of control plane than that of cross plane submarines. In this study, captive model tests were conducted to evaluate the maneuverability of an X-plane submarine using Computational Fluid Dynamics (CFD) and a mathematical maneuvering model. For CFD analysis, SNUFOAM, CFD software specialized in naval hydrodynamics based on the open-source toolkit, OpenFOAM, was applied. A generic submarine Joubert BB2 was selected as a test model, which was modified by Maritime Research Institute Netherlands (MARIN). Captive model tests including propeller open water, resistance, self-propulsion, static drift, horizontal planar motion mechanism and vertical planar motion mechanism tests were carried out to obtain maneuvering coefficients of the submarine. Maneuvering simulations for turning circle tests were performed using the maneuvering coefficients obtained from the captive model tests. The simulated trajectory showed good agreement with that of free running model tests. From the results, it was proved that CFD simulations can be applicable to obtain reliable maneuvering coefficients for X-plane submarines.

평면트러스로 지지된 리프트 게이트의 진동특성 (Dynamic Characteristic of Lift Gate Supported by Plane Truss)

  • 이성행;양동운;함형길;공보성;신동욱
    • 한국농공학회논문집
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    • 제54권3호
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    • pp.133-139
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    • 2012
  • Dynamic characteristic of lift gate supported by plane truss is studied by a model test scaled with the ratio of 1 : 31.25 in the four major rivers project. The vibrations of gate supported by the plane truss is assessed in comparison with those of gate supported by the space truss which was tested formerly. The gate model is made of acryl panel and calibrated by lead. A model test is conducted under the different gate opening and upstream water levels conditions in the concrete test flume dimensioned 1.6 m in width, 0.8 m in height and 24 m in length. In order to verify the model, natural frequencies of the model gate are measured, and compared with the numerical results. The vibrations of gate model supported by the plane truss in opening height of 1.0 cm~2.0 cm shows greater than one supported by the space truss. It is found that the gate model supported by the plane truss is less desirable than one supported by the space truss. thus, the latter type of gate model is requested to design.

피라노미터 실측 일조량을 통한 직산 분리 모델과 경사면 일조량 변환 모델에 관한 연구 (A Research on the Decomposition Model and Transposition Model Using the Measured Pyranometer Irradiation Data)

  • 이상혁;이경수
    • 한국태양에너지학회 논문집
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    • 제38권3호
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    • pp.1-20
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    • 2018
  • It is a very important and fundamental process to know accurately the intensity of the solar energy coming into the installed module considering the tilted angle. Europe and the US commonly use a program called PVsyst to convert the global horizontal irradiation to global irradiation on tilted plane. There are two types of models that PVsyst uses to convert to irradiation on tilted plane. In this paper, Perez model, which is a decomposition model and Perez model, which is a transposition model used in PVsyst, are applied based on global horizontal irradiation and global irradiation on tilted plane measured in a specific area. The comparison of the decomposition model shows the effect of the transpostion model on global irradiation on tilted plane conversion by comparing the ratio of the horizontal diffuse irradiation amount of the Watanabe model which are highly trusted in Asia and the Perez model. The comparison of transposition model confirm the error between the measured data and the calculated value which is applied Perez model to global horizontal irradiation decomposed by Perez model and Watanabe model. Based on the two comparisons, This paper propose a method to confirm the reliability of transposition model and reduce the error when PVsyst is used in Korea.

차체 외부에서의 유동해석 (Flow Analysis on the Outside of Automotive Body)

  • 조재웅;한문식
    • 한국기계가공학회지
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    • 제9권1호
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    • pp.55-60
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    • 2010
  • The air resistance about automotive body is studied by the flow analysis in this study. Maximum air flow velocity is shown with 28 to 30 m/s on the upper roof of automotive body. The air flow becomes most regular at automotive body model 3 but the model of 2 or 3 becomes irregular in comparison with the model 1. The maximum air resistance pressure is shown with 413 to 420 Pa at the front bumper of automotive body. The flow velocity at inlet or middle plane of automotive body is shown as the contour same with the model of 1, 2, or 3. But the velocity at outlet plane at model 1 is shown as the contour different with the model of 2 or 3.

Variation simulation and diagnosis considering in-plane/out-of-plane welding distortion

  • Lee, Hyeonkyeong;Chung, Hyun
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제11권1호
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    • pp.553-571
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    • 2019
  • Geometric variation including welding distortion accumulates as many parts are joined together, ultimately affecting the final product. This variation is then subjected to correction, which requires considerable effort, time, and cost. This variation can be categorized as in-plane/out-of-plane variation. To date, studies on variation simulation have largely focused on the out-of-plane variation, however the variation generated in the in-plane direction requires more time and efforts to correct afterwards. This research aims to construct a variation simulation model considering both the in-plane and out-of-plane variations. A geometric analysis was performed to derive an equation that reflects the coupling effect of the out-of-plane variation on the in-plane variation. The proposed model is validated with case study analysis and the results shows that good fidelity in predicting and diagnosing the in-plane variation during the block assembly process considering welding distortion.

입자와 섬유로 보강된 SMC 복합재의 기계적 특성에 관한 연구 (Mechanical Properties of Particle and Fiber Reinforced SMC Composites)

  • 정현조;윤성호
    • 한국자동차공학회논문집
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    • 제4권2호
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    • pp.173-182
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    • 1996
  • An analytical model has been developed to predict the elastic properties of a filled resin reinforced by chopped fibers, a three-phase composite such as a filled sheet molding compound(SMC). In the model the matrix material and fillers form an effective matrix. The effective matrix is then considered to be reinforced with long fibers lying in the sheet plane but randomly oriented in the plane. Expressions for the resulting transversely isotropic composite properties are explicitly presented. Using this model, the Young's and shear moduli are calculated for the SMC sample with filler weight fraction of 35% and fiber content of 30%. The same properties are also determined experimentally. The agreement between the calculated and measured elastic moduli is found to be very good for the in-plane properties. However, the out-of-plane properties show a large difference because the effect of voids is not taken into account in the model.

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구형 도파관 모델에 의한 직사각형 전원평면의 임피던스 계산 (Impedance Calculation of the Rectangular Power Plane by the Waveguide Model)

  • 박면주;이병제
    • 한국전자파학회논문지
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    • 제15권12호
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    • pp.1147-1151
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    • 2004
  • 본 논문에서는 직사각형 전원평면에 대한 새로운 해석적 모델과 그에 기반한 임피던스 표현식을 제시하였다. 제안된 방법에서는 전원평면 구조를 그 둘레에 적당한 경계 조건을 가지는 일정 길이의 직사각형 도파관으로 모델화 하였다. 그 결과 제안된 모델에 기반하여 유도된 임피던스 표현식이 1차원 급수형태로 나타나며, 이는 기존에 제안된 전원평면의 구형 공동 모델에 기반한 임피던스 식에 비해 계산 효율을 크게 높일 수 있다.

3차원 대칭단면 유동장에서의 개선된 난류모델 (Improved Turbulence Model on the 3 Dimensional Plane of Symmetry Flow)

  • 손창현
    • 한국전산유체공학회지
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    • 제2권2호
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    • pp.1-8
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    • 1997
  • Two versions of anisotropic k-ε turbulence model are incorporated in the modified k-ε model of Sohn et al. to avoid the need for the experimental normal stress value in the model and applied to convergent and divergent flows with strong and adverse pressure gradients in the plane of symmetry of a body of revolution. The models are the nonlinear k-ε model of Speziale and the anisotropic model of Nisizima & Yoshizawa. All of the models yield satisfactory results for relatively complex flow on a plane-of-symmetry boundary layer. The results of the models are compared with those results of experimental normal stress value.

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한국인 정상교합자의 악태모형위에서의 안와평면과 상악견치 사이의 거리 (THE DISTANCE BETWEEN THE UPPER CANINE AND THE ORBITAL PLANE IN GNATHOSTATIC MODEL OF KOREANS WITH NORMAL OCCLUSION)

  • 이수인;최목균;김광현
    • 대한치과교정학회지
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    • 제5권1호
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    • pp.51-56
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    • 1975
  • In orthodontic field, the study on gnathostatic model is very important to the diagnosis and analysis of malocclusion. The purpose of this study is to observe that relation of orbital plane and upper canine in Koreans. We selected 230 cases with normal occlusion, 124 male and 106 female cases aged from 12 years to 25 years, to prepare 230 gnathostatic models, and measured the distance from midpoint of mesio-distal distance of upper canine to orbital plane in gnathostatic model. The results obtained were as follows: 1) The mean value of the distance from upper canine to orbital plane showed no significant change with age. 2) The mean value of the distance from the upper canine to orbital plane was -3.11mm in male and -3.84mm in female. 3) The orbital plane passed through the upper canine in normal occlusion of Koreans.

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