• 제목/요약/키워드: parameter sweep

검색결과 30건 처리시간 0.038초

2-변수 모션기반의 스윕곡면 (A Sweep Surface based on Two-Parameter Motion)

  • 윤승현;이지은
    • 한국컴퓨터그래픽스학회논문지
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    • 제17권1호
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    • pp.1-7
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    • 2011
  • 본 논문에서는 2-변수 모션 (two-parameter motion)을 이용한 새로운 스윕곡면의 생성 및 편집기법을 제시한다. 먼저, 하나의 변수로 매개화되는 기존의 모션에서 방향곡선 (orientation curve)과 크기 변환곡선 (scaling curve)을 곡면의 형태로 확장한 2-변수 모션의 개념을 소개하고, 이를 이용한 새로운 스윕곡면을 제안한다. 제안된 스윕곡면은 하나의 정점이 2-변수 모션에 적용된 결과이며, u-방향의 등위곡선 (iso-curve)이 매개변수 ${\upsilon}$에 따라 다른 형상을 갖게된다. 또한 이에 대한 효율적인 모델링 및 편집기법은 2-변수모션의 직관적인 제어를 통해서 이루이진다. 본 논문에서는 복잡한 형상에 대한 모델링 및 편집 실험을 통해서 제안된 기법의 효율성 및 편리성을 입증한다.

마이크로스트립 패치 안테나 설계에서 타구치 직교배열표의 유용성 분석 (Analysis for Usefulness of Taguchi's Orthogonal Array in Microstrip Patch Antenna Design)

  • 김재연;장대순;허정
    • 한국인터넷방송통신학회논문지
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    • 제19권4호
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    • pp.41-46
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    • 2019
  • 타구치 직교배열표를 활용하여 마이크로스트립 패치 안테나 설계를 효율적으로 수행 가능한지를 분석하였다. 비교 및 분석을 위하여 U-슬롯 마이크로스트립 패치 안테나에서 U-슬롯의 모양과 변형된 급전부의 요소를 파라미터로 정했다. 해당 파라미터들의 스윕을 통해 도출된 모든 시뮬레이션의 결과와 타구치의 직교배열표를 이용하여 도출된 축소 시뮬레이션 결과를 비교분석하였다. 파라미터 스윕을 이용하여 진행된 19,683회의 시뮬레이션을 타구치의 직교배열표를 이용한 27번의 시뮬레이션으로 대폭 축소하였으며, 파라미터 스윕과 직교배열표를 이용한 시뮬레이션의 평균 10dB 대역폭은 3.7%의 오차를 가진다. 따라서, 시뮬레이션 횟수를 줄이고도 효율적으로 안테나 파라미터 특성을 파악할 수 있음을 확인했다.

축류형 홴 성능 및 소음에 영향을 미치는 설계변수 분석 (Design Parameter Analysis on the Performance and Noise of Axial Fan)

  • 김기황;이승배;주재만
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 추계학술대회논문집 I
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    • pp.275-281
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    • 2001
  • While basic input parameters for the performance and noise of axial fan are flow rate, pressure rise, rotating speed, and fan diameter, the geometric parameters of blade are sweep angle, solidity, and camber angle. The sweep angle does not affect fan performance much, but on fan noise significantly. Solidity and camber angle are very critical design parameters acting on the fan performance directly. The solidity and camber angle are closely related, therefore they have to be carefully determined for the low-noise and high-performance fan. In This paper, different design points are selceted and also geometric parameters are deliberately changed for the comparison of fan noise. As a result, at the same performance, the input rotational speed affects radiated noise more significantly than others. When solidity and camber angle are increased more than those by iDesignFan/sup TM/ program, more noise is experienced. The blade sweep method and blade numbers at same solidity are observed to results in different levels of performance and noise.

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Lateral torsional buckling of steel I-beams: Effect of initial geometric imperfection

  • Bas, Selcuk
    • Steel and Composite Structures
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    • 제30권5호
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    • pp.483-492
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    • 2019
  • In the current study, the influence of the initial lateral (sweep) shape and the cross-sectional twist imperfection on the lateral torsional buckling (LTB) response of doubly-symmetric steel I-beams was investigated. The material imperfection (residual stress) was not considered. For this objective, standard European IPN 300 beam with different unbraced span was numerically analyzed for three imperfection cases: (i) no sweep and no twist (perfect); (ii) three different shapes of global sweep (half-sine, full-sine and full-parabola between the end supports); and (iii) the combination of three different sweeps with initial sinusoidal twist along the beam. The first comparison was done between the results of numerical analyses (FEM) and both a theoretical solution and the code lateral torsional buckling formulations (EC3 and AISC-LRFD). These results with no imperfection effects were then separately compared with three different shapes of global sweep and the presence of initial twist in these sweep shapes. Besides, the effects of the shapes of initial global sweep and the inclusion of sinusoidal twist on the critical buckling load of the beams were investigated to unveil which parameter was considerably effective on LTB response. The most compatible outcomes for the perfect beams was obtained from the AISC-LRFD formulation; however, the EC-3 formulation estimated the $P_{cr}$ load conservatively. The high difference from the EC-3 formulation was predicted to directly originate from the initial imperfection reduction factor and high safety factor in its formulation. Due to no consideration of geometric imperfection in the AISC-LFRD code solution and the theoretical formulation, the need to develop a practical imperfection reduction factor for AISC-LRFD and theoretical formulation was underlined. Initial imperfections were obtained to be more influential on the buckling load, as the unbraced length of a beam approached to the elastic limit unbraced length ($L_r$). Mode-compatible initial imperfection shapes should be taken into account in the design and analysis stages of the I-beam to properly estimate the geometric imperfection influence on the $P_{cr}$ load. Sweep and sweep-twist imperfections led to 10% and 15% decrease in the $P_{cr}$ load, respectively, thus; well-estimated sweep and twist imperfections should considered in the LTB of doubly-symmetric steel I-beams.

관류형팬의 설계변수 특성에 관한 연구 (A Study on Characteristics of Design Parameters for In-line Duct Fan)

  • 박진욱;허종철;이철형;박완순
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.373-377
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    • 2005
  • The Performance of in-line duct fan depends on the design parameters of impeller and guide vane. such as sweep back angle of impeller, the number of blades, outlet blade angle, guide vane angle etc. In this experimental study total four kinds of impellers having different sweep back angles, $90^{\circ},\;72.5^{\circ},\;55^{\circ},\;37.5^{\circ}$ with 8 guide vanes, different the number of blades, 6ea, 8ea, 10ea, 12ea, different kinds of outlet blade angles, $30^{\circ},\;45^{\circ}.\;60^{\circ}$ and different kinds of guide vane angles, $15^{\circ},\;30^{\circ},\;45^{\circ}$ were selected and their performance measured to investigate the effects of them. The results were non-dimensionalized to compare their performance.

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The Algorithm of Sweep-the-Negatives and its Applications to Order Resticted Inference

  • Kim, Byong-Dok;Park, Jae-Rong;Akio Kudo
    • Journal of the Korean Statistical Society
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    • 제19권1호
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    • pp.54-70
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    • 1990
  • Consider the extreme problem : min$(\mu-y)'(\mu-y)$ subject to $A\mu \geq 0$, where A is an $n \times p$ matrix, which often occurs in solving the maximum likelihood estimator with ordered restrictions in parameter space. In case the matrix AA' has all non-positive off-diagonal elements, some propositions in this paper guarantee that the above extreme solutions are achieved at most at n sweep out steps in Gaussian eliminations. Some typicla examples of Sweep-the-Negatives method are given.

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호모토피 알고리즘을 이용한 Successive Backward Sweep 최적제어 알고리즘 설계 및 궤도전이 문제에의 적용 (Successive Backward Sweep Method for Orbit Transfer Augmented with Homotopy Algorithm)

  • 조동현;김승필
    • 한국항공우주학회지
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    • 제44권7호
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    • pp.620-628
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    • 2016
  • 호모토피 알고리즘은 비선형성이 강하거나 다수의 최적해가 존재하는 비선형 최적제어 문제에서 점진적으로 비선형 항으로 고려하게 해줌으로써 강건하게 전역의 최적해를 구할 수 있는 방법이다. 본 논문에서는 초기 추정치에 둔감한 SBS 알고리즘과 호모토피 알고리즘을 결합한 비선형 최적제어 알고리즘을 제시하였다. 이러한 접근방식은 저추력 궤적최적화 문제와 같이 비선형성이 강한 문제의 최적해를 구하는데 효과적이다. 또한, 비선형성이 강한 문제들은 종종 다수 국소 해가 존재하게 되는데, 이러한 경우에 SBS-호모토피 방법은 점진적으로 전역해를 찾는 것을 가능하게 한다.

직접접촉식과 동반기체식 막증류 공정의 투과수 변화에 따른 비교해석 (Permeate Flux Analysis of Direct Contact Membrane Distillation (DCMD) and Sweep Gas Membrane Distillation (SGMD))

  • 엄수환;;이용택
    • 멤브레인
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    • 제21권3호
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    • pp.236-246
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    • 2011
  • 본 연구에서는 기공의 크기가 $0.4{\mu}m$의 소수성 막인 폴리에틸렌 100가닥으로 모듈을 제작하여 직접접촉식과 동반기체식 막증류 과정에서 막의 양단의 온도차, 공급수의 염분농도, 그리고 냉각수/동반기체의 유량에 대해서 투과수의 플럭스를 측정하였다. 이론적으로는, 동반기체식 막증류는 직접접촉식 막증류 공정의 막의 투과측 표면과 냉각수 사이에 동반 기체층이 추가된 것으로 간주하였다. 이 동반기체층은 새로운 저항층과과 동반기체의 이동중 상변화된 수증기가 손실되는 것이 투과유속을 30% 정도 감소시키게 된다. 물질수지식을 이용하여, 기존의 식과는 다르게 보정계수(${\omega}$)를 넣어 직접접촉식 막증류와 동반기체식 막증류의 이론값을 실험값과 비교 분석하였다.

A parameter sweep approach for first-cut design of 5 MW Ship propulsion motor

  • Bong, Uijong;An, Soobin;Im, Chaemin;Kim, Jaemin;Hahn, Seungyong
    • 한국초전도ㆍ저온공학회논문지
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    • 제21권1호
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    • pp.25-30
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    • 2019
  • This paper presents a conceptual design approach of air-cored synchronous machine with high temperature superconductor (HTS) field winding. With a given configuration of a target machine, boundary conditions are set in the cylindrical coordinate system and analytic field calculation is performed by solving a governing equation. To set proper boundary conditions, current distributions of the field winding and the armature winding are expressed by the Fourier expansion. Based on analytic magnetic field calculation results, key machine parameters are calculated: 1) inductance, 2) critical current of field winding, 3) weight, 4) HTS conductor consumption, and 5) efficiency. To investigate all potential design options, 6 sweeping parameters are determined to characterize the geometry of the machine and the parameter calculation process is performed for each design options. Among design options satisfying constraints including >80 % critical current margin and >95 % efficiency, in this paper, a first-cut design was selected in terms of overall machine weight and HTS conductor consumption to obtain a lightweight and economical design. The goal is to design a 5-MW machine by referring to the same capacity machine that was previously constructed by another group. Our design output is compared with finite element method (FEM) simulation to validate our design approach.

트랜스퍼 금형에 있어서 IC 폐키지의 성형 유동 해석에 관한 연구 (A Study on the Molding Analysis of IC Package in Transfer mold)

  • 구본권
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 1995년도 추계학술대회 논문집
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    • pp.64-67
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    • 1995
  • Transfer Molding is currently the most widely used process for encapsulation integrated circuits(;IC). Although the process has been introduced over 20 years ago, generating billions of parts each year, it is far from being optimized. With each new mold, epoxy mold, epoxy mold compound, and lead-frame, lengthy period and expensive qualification runs have to be performed to minimized defects ranging from wire sweep, incomplete fill, and internal voids etc. This studies describes how simulation can be applied to transfer molding to yield acceptable design and processing parameter. The non-isothermal filling of non-newtonian reactive epoxy molding compound(;EMC) in a multi-cavity mold is analyzed. Sensitivity analysis is conducted to investigate the influence of process deviations on the final molded profile. This study trend is carried out by following some heuristic process guidelines.

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