• 제목/요약/키워드: Surface geometry

검색결과 1,291건 처리시간 0.028초

반응면 기법을 이용한 자동차 엔진 냉각팬의 저소음설계 (Optimization of Automotive Engine-cooling Fan Noise Using Response Surface Method)

  • 이정한;안재권;이수갑
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.407-412
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    • 2000
  • Response surface method is employed in optimizing the acoustic performance of automotive engine-cooling axial fans. The effects of modifications in blade geometry on noise reduction are investigated. Taking the far-field noise level as the objective, a quadratic response surface is constructed utilizing D-Optimality condition as the candidate-points selection criteria. It is shown that the quadratic model exhibits an excellent fitting capability resulting in the blade design with low far-field noise level.

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Heat and mass transfer processes at the most heat-stressed areas of the surface of the descent module

  • Oleg A., Pashkov;Boris A., Garibyan
    • Advances in aircraft and spacecraft science
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    • 제9권6호
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    • pp.493-506
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    • 2022
  • The study presents the results of the research of heat and heat exchange processes on the heat-stressed elements of the structure of an advanced TsAGI descent vehicle. The studies were carried out using a mathematical model based on solving discrete analogs of continuum mechanics equations. Conclusions were drawn about the correctness of the model and the dependence of the intensity of heat and mass transfer processes on the most heat-stressed sections of the apparatus surface on its geometry and the catalytic activity of the surface.

다목적실용위성 3호의 지표 정규식생지수 산출 및 비교 분석: GeoEye 자료 활용 (The comparative analysis of KOMPSAT-3 based surface normalized difference vegetation index: Application of GeoEye data)

  • 염종민
    • 항공우주기술
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    • 제13권2호
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    • pp.80-86
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    • 2014
  • 본 연구에서는 다목적실용위성 3호 영상을 이용하여 지표면 상의 정규식생지수 비교 분석 하고자 한다. 산출된 다목적실용위성 3호의 정규식생지수 비교 분석을 위해 동일 지점 최소 관측 시간 오차를 가지는 고해상도 GeoEye 영상이 사용되었다. 먼저, 각 밴드별 분광 정도 산출을 위해 대기 보정이 수행되었다. 대기 보정 수행을 위한 기하 정보는 다목적실용위성 3호 보조자료에 포함된 태양천정각, 태양방위각, 위성천정각, 위성방위각, 날짜 정보이다. 그리고 대기 요소에 의한 감쇄, 산란, 흡수 정보를 물리적으로 계산하기 위해 수증기량, 오존량, 에어러솔 정보가 적용되었다. 일반적으로 정확한 대기정보를 얻기 위해서는 현장관측자료가 중요하지만, 본 연구에서는 MODIS atmospheric products를 사용하였고, 대기보정 모델에서 산출된 지면 반사도는 식생지수 산출에 사용되었다.

TiO2 나노튜브 형상에 미치는 NH4F와 H2O의 영향 (Effects of NH4F and H2O on the Geometry of TiO2 Nanotubes)

  • 김건두;장상순;김희산
    • Corrosion Science and Technology
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    • 제17권3호
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    • pp.138-145
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    • 2018
  • The aim of this work is the attainment of the $TiO_2-nanotube$ photocatalytic-growth condition using anodization, whereby the $NH_4F-H_2O$ weight ratio is appropriately controlled. We fabricated the $TiO_2$ nanotubes using a two-step anodization (first step is 1 hr; second step is 30 hr) under the ambient pressure and the room temperature at 60 V in ethylene-glycol solutions to investigate the effects of the $NH_4F$(0.1,0.3,0.5wt%) and $H_2O$(1-3wt%) on the $TiO_2-nanotube$ geometry and the photocatalytic efficiency. Further, the decomposition efficiency of the methylene blue on the $TiO_2$ nanotubes by the UN radiation depended on the geometrical change of the nanotube geometry, indicating the proportionality of the decomposition efficiency to the surface area that was affected by the $NH_4F$ and $H_2O$ concentrations. As the $NH_4F$ weight was increased, the surface area initially decreased but slightly increased later, and the length consistently increased. As the $H_2O$ weight was increased, the surface area and length initially increased, but later decreased with the 3 wt% $H_2O$.

An optimal design of wind turbine and ship structure based on neuro-response surface method

  • Lee, Jae-Chul;Shin, Sung-Chul;Kim, Soo-Young
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제7권4호
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    • pp.750-769
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    • 2015
  • The geometry of engineering systems affects their performances. For this reason, the shape of engineering systems needs to be optimized in the initial design stage. However, engineering system design problems consist of multi-objective optimization and the performance analysis using commercial code or numerical analysis is generally time-consuming. To solve these problems, many engineers perform the optimization using the approximation model (response surface). The Response Surface Method (RSM) is generally used to predict the system performance in engineering research field, but RSM presents some prediction errors for highly nonlinear systems. The major objective of this research is to establish an optimal design method for multi-objective problems and confirm its applicability. The proposed process is composed of three parts: definition of geometry, generation of response surface, and optimization process. To reduce the time for performance analysis and minimize the prediction errors, the approximation model is generated using the Backpropagation Artificial Neural Network (BPANN) which is considered as Neuro-Response Surface Method (NRSM). The optimization is done for the generated response surface by non-dominated sorting genetic algorithm-II (NSGA-II). Through case studies of marine system and ship structure (substructure of floating offshore wind turbine considering hydrodynamics performances and bulk carrier bottom stiffened panels considering structure performance), we have confirmed the applicability of the proposed method for multi-objective side constraint optimization problems.

FEM을 이용한 RECTANGULAR CAN 후방압출 해석 (Rectangular can backward extrusion analysis using FEM)

  • 이상승;조규종
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2001년도 춘계학술대회 논문집
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    • pp.699-702
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    • 2001
  • The increasing demand in industry to produce rectangular cans at the reduction by the rectangular backward extrusion process involves better understanding of this process. In 2-D die deflection and dimensional variation of the component during extrusion, punch retraction, component injection and cooling was conducted using a coupled thermal-mechanical approach for the forward extrusion of aluminum alloy and low-carbon steel in tools of steel. Backward extrusion FE simulation and experimental simulation by physical modeling using wax as a model material have been performed. These simulations gave good results concerning the prediction of th flow modes and the corresponding surface expansions of the material occuring at the contact surface between the can and the punch. There prediction are the limits of the can height, depending on the reduction, the punch geometry, the workpiece material and the friction factor, in order to avoid the risk of damage caused by sticking of the workpiece material to the punch face. The influence of these different parameter on the distribution of the surface expansion along the inner can wall and bottom is already determined. This paper deals with the influence of the geometry changes of the forming tool and the work material in the rectangular backward using the 3-D finite element method.

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미세입자 분사가공을 위한 3 차원 임의형상 모재용 마스크 모델링 (Mask Modeling of a 3D Non-planar Parent Material for Micro-abrasive Jet Machining)

  • 김호찬;이인환;고태조
    • 한국정밀공학회지
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    • 제27권8호
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    • pp.91-97
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    • 2010
  • Micro-abrasive Jet Machining is one of the new technology which enables micro-scale machining on the surface of high brittle materials. In this technology it is very important to fabricate a mask that prevents excessive abrasives not to machine un-intend surface. Our previous work introduced the micro-stereolithography technology for the mask fabrication. And is good to not only planar material but also for non-planar materials. But the technology requires a 3 dimensional mask CAD model which is perfectly matched with the surface topology of parent material as an input. Therefore there is strong need to develop an automated modeling technology which produce adequate 3D mask CAD model in fast and simple way. This paper introduces a fast and simple mask modeling algorithm which represents geometry of models in voxel. Input of the modeling system is 2D pattern image, 3D CAD model of parent material and machining parameters for Micro-abrasive Jet Machining. And the output is CAD model of 3D mask which reflects machining parameters and geometry of the parent material. Finally the suggested algorithm is implemented as software and verified by some test cases.

보행자 보호를 위한 안전 후드 개발 (Development of Safe Hood for Pedestrian Protection)

  • 김태정;홍승현;이두환;한도석
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2008년도 춘계학술대회 논문집
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    • pp.345-346
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    • 2008
  • Most pedestrian-vehicle crashes involve frontal impacts, and the vehicle front structures are responsible for most pedestrian injuries. The vehicle bumper contacts the lower legs at first. The leading edge of the hood (bonnet) strikes the proximal upper leg and finally, the head and upper torso hit the top surface of the hood or windscreen. In essence, the pedestrian wraps around the front of the vehicle until pedestrian and vehicle are traveling at the same speed. Since the hood surface is made from sheet metal, it is a relatively compliant structure and does not pose a major risk for severe head trauma. However, serious head injury can occur when the head hits a region of the hood with stiff underlying structures such as engine components. The solution is to provide sufficient clearance between the hood and underlying structures for controlled deceleration of a pedestrian's head. However, considerations of aerodynamic design and styling can make it extremely difficult to alter a vehicle's front end geometry to provide more under-hood space. In this study, the safe hood will be developed by designing new conceptual inner panel in order to decrease the pedestrian's head injuries without changing hood outer geometry.

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3차원 균열을 갖는 구조물에 대한 건전성 평가(I) (Integrity Evaluation for 3D Cracked Structures(I))

  • 이준성
    • 한국산학기술학회논문지
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    • 제13권8호
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    • pp.3295-3300
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    • 2012
  • 3차원 유한요소법은 구조물에 존재하는 표면균열과 내재균열들의 응력확대계수를 구하는데 이용되어 진다. 기하모델, 즉 솔리드모델은 3차원 균열들을 포함하고 있다. 국부적인 절점밀도가 선택되어 지면 자동적으로 기하모델 영역에 중첩되어 지며 절점은 버블패깅 방법에 의해 생성되어지고 10절점 사변형 솔리드요소는 데라우니 삼각화 기술에 의해 생성하였다. 시스템의 정확도와 효용성을 체크하기 위해 인장하중을 받는 평판에 하나의 균열이 존재하는 경우의 응력확대계수를 구해 Raju-Newnam식과 비교하여 5%이내의 차이를 보였다. 또한, 인장하중을 받는 평판에 두개 균열이 존재하는 경우의 해석을 통해 상호 간섭 효과를 분석하였다.

IGNITION OF REACTIVE SOLIDS WITH ROUGH SURFACE BY CONSTANT HEAT FLUX

  • Chae, J.O.;Mokhin, G.N.;Moon, J.I.;Shmelev, V.M.
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1995년도 제5회 학술강연회논문집
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    • pp.11-30
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    • 1995
  • The ignition characteristics of a reactive solid with rough surface by constant heat flux were studied. The geometry of surface was represented by a set of identical protrusions having a shape of wedge based on the block of reactive solid. Several regimes of ignition were found, depending on the ratio of the protrusion length and the depth of the heated layer, formed in course of ignition process: 1) when the substance is ignited as the massive block, and the effect of roughness is not pronounced; 2) when ignited are the individual protrusions; and 3) in the intermediate region between the first two. Critical ignition conditions: ignition time and ignition criterion, are determined for the three regimes. The results are compared with the results for the one-dimensional ignition of the semi-infinite body. It is shown, that the effect of geometry on ignition results in the considerable reduction of ignition delay, and the amount of energy required for the successful ignition is less compared to the one- dimensional case.

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