• 제목/요약/키워드: parametric functions

검색결과 277건 처리시간 0.023초

Bending behavior of microfilaments in living cell with nonlocal effects

  • Muhammad Safeer;Muhammad Taj;Mohamed A. Khadimallah;Muzamal Hussain;Saima Akram;Faisal Mehmood Butt;Abdelouahed Tounsi
    • Advances in nano research
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    • 제15권1호
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    • pp.15-23
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    • 2023
  • Dynamics of protein filamentous has been an active area of research since the last few decades as the role of cytoskeletal components, microtubules, intermediate filaments and microfilaments is very important in cell functions. During cell functions, these components undergo the deformations like bending, buckling and vibrations. In the present paper, bending and buckling of microfilaments are studied by using Euler Bernoulli beam theory with nonlocal parametric effects in conjunction. The obtained results show that the nonlocal parametric effects are not ignorable and the applications of nonlocal parameters well agree with the experimental verifications.

자동차 현가 및 조향 장치 부품설계 자동화 시스템 개발 (Development of An Automated Design System for Suspension and Steering parts)

  • 이광일;정승용;조희봉;강재관
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2002년도 춘계학술대회 논문집
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    • pp.352-356
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    • 2002
  • In this paper, an automated design system of suspension and steering parts is developed. The system automates the processes of 3-D modeling and 2-D drafting of the parts. In addition, the BOM and dimension data of the designed part is also automatically transferred to the database of ERP system. The system is developed by using the functions of parametric design and API(application Programming Interface) of the a commercial solid modeler.

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조경 설계 분야에서 파라메트릭 디자인의 사례 분석과 활용 가능성 (Case Analysis and Applicability Review of Parametric Design in Landscape Architectural Design)

  • 나성진
    • 한국조경학회지
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    • 제49권2호
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    • pp.1-16
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    • 2021
  • 조경의 설계 행위는 설계가의 사고체계 내에서 형성되는 개념과 그것이 형상화되는 구체적인 재현 그리고 이를 실질적인 재료로 구축하는 일련의 과정으로 이루어지며, 이러한 디자인 프로세스는 4차 산업혁명 시대의 컴퓨터 기술과 IT 생태계의 비약적인 발전으로 많은 변화를 마주하고 있다. 컴퓨터 테크놀로지는 산업 초기에 수학적 계산(calculation)과 입력 데이터의 시각적 표현(graphic representation on display) 등 비교적 단순한 목적으로 개발되었다. 하지만 ibm과 매킨토시(macintosh)를 시작으로 개인용 컴퓨터(personal computer)의 성공적인 보급 이후 프로그램 언어와 하드웨어가 급속히 발전하고, 알고리즘(algorithm) 및 응용 소프트웨어가 전문화되면서 컴퓨터의 활용 목적이 사회 전반에 걸쳐 매우 다양해졌다. 본 연구는 이러한 디지털 사회 맥락의 변화를 바탕으로 컴퓨테이셔널 디자인(computational design), 파라메트릭 디자인(parametric design) 및 알고리즘 디자인(algorithm design) 등의 새로운 설계 방법들이 조경 설계 과정에서 어떠한 기능과 역할을 할 수 있는지에 관한 현황 및 쟁점을 진단하였으며, 그중 최근 가장 주목받는 파라메트릭 테크놀로지를 적극적으로 이용하는 디자인 방법론에 집중해 연구를 진행했다. 우선 현대 조경 및 건축 전반에서 파라메트릭 디자인의 주요 개념 및 특징들에 대해 살펴 논의의 근거를 마련했다. 그리고 이를 바탕으로 조경 분야에서 파라메트릭 디자인 활용에 관한 선행 연구를 분석하고, 조경 설계 회사들의 실제 활용 현황에 대해 분석했다. 그 결과, 조경 분야에서 파라메트릭 디자인 활용에 관한 연구는 연구의 수나 다양성 측면에서 타 분야와 비교했을 때 아직 충분한 논의가 진행되지 않은 것을 확인할 수 있었고, 사용 현황 분석에서는 최근 국외 조경 회사들을 중심으로 새로운 테크놀로지를 적극적으로 활용하려는 다양한 움직임이 조사되었다. 마지막으로 이러한 논의를 바탕으로 조경 설계 분야에서 파라메트릭 디자인 활용의 구체적인 사례 및 추후 다양한 가능성에 대해 검토했다.

Parametric resonance of composite skew plate under non-uniform in-plane loading

  • Kumar, Rajesh;Kumar, Abhinav;Panda, Sarat Kumar
    • Structural Engineering and Mechanics
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    • 제55권2호
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    • pp.435-459
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    • 2015
  • Parametric resonance of shear deformable composite skew plates subjected to non-uniform (parabolic) and linearly varying periodic edge loading is studied for different boundary conditions. The skew plate structural model is based on higher order shear deformation theory (HSDT), which accurately predicts the numerical results for thick skew plate. The total energy functional is derived for the skew plates from total potential energy and kinetic energy of the plate. The strain energy which is the part of total potential energy contains membrane energy, bending energy, additional bending energy due to additional change in curvature and shear energy due to shear deformation, respectively. The total energy functional is solved using Rayleigh-Ritz method in conjunction with boundary characteristics orthonormal polynomials (BCOPs) functions. The orthonormal polynomials are generated for unit square domain using Gram-Schmidt orthogonalization process. Bolotin method is followed to obtain the boundaries of parametric resonance region with higher order approximation. These boundaries are traced by the periodic solution of Mathieu-Hill equations with period T and 2T. Effect of various parameters like skew angle, span-to-thickness ratio, aspect ratio, boundary conditions, static load factor on parametric resonance of skew plate have been investigated. The investigation also includes influence of different types of linearly varying loading and parabolically varying bi-axial loading.

Parametric numerical study of wind barrier shelter

  • Telenta, Marijo;Batista, Milan;Biancolini, M.E.;Prebil, Ivan;Duhovnik, Jozef
    • Wind and Structures
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    • 제20권1호
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    • pp.75-93
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    • 2015
  • This work is focused on a parametric numerical study of the barrier's bar inclination shelter effect in crosswind scenario. The parametric study combines mesh morphing and design of experiments in automated manner. Radial Basis Functions (RBF) method is used for mesh morphing and Ansys Workbench is used as an automation platform. Wind barrier consists of five bars where each bar angle is parameterized. Design points are defined using the design of experiments (DOE) technique to accurately represent the entire design space. Three-dimensional RANS numerical simulation was utilized with commercial software Ansys Fluent 14.5. In addition to the numerical study, experimental measurement of the aerodynamic forces acting on a vehicle is performed in order to define the critical wind disturbance scenario. The wind barrier optimization method combines morphing, an advanced CFD solver, high performance computing, and process automaters. The goal is to present a parametric aerodynamic simulation methodology for the wind barrier shelter that integrates accuracy and an extended design space in an automated manner. In addition, goal driven optimization is conducted for the most influential parameters for the wind barrier shelter.

반응표면법을 이용한 구조물 최적설계 프로그램의 개발 (Development of a Structural Optimal Design Code Using Response Surface Method Implemented on a CAD Platform)

  • 염기선;허재성;곽병만
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집C
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    • pp.580-585
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    • 2001
  • A response surface method(RSM) is utilized for structural optimization and implemented on a parametric CAD platform. Once an approximation of the performance function is made, no formal design sensitivity analysis is necessary. The approximation gives the designer the sensitivity information and furthermore intuition on the performance functions. The scheme for the design of experiment chosen for the RSM has a large influence on the accuracy of converged solutions and the amount of computation. The D-optimal design criterion as implemented in this paper is found efficient for the structural optimization. The program is developed on a parametric CAD platform and tested using several shape design problems of such as a torque arm and a belt clip. It is observed that the RSM used provides a faster convergence than other approximation methods for design sensitivity.

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Application of Fuzzy Information Representation Using Frequency Ratio and Non-parametric Density Estimation to Multi-source Spatial Data Fusion for Landslide Hazard Mapping

  • Park No-Wook;Chi Kwang-Hoon;Kwon Byung-Doo
    • 한국지구과학회지
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    • 제26권2호
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    • pp.114-128
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    • 2005
  • Fuzzy information representation of multi-source spatial data is applied to landslide hazard mapping. Information representation based on frequency ratio and non-parametric density estimation is used to construct fuzzy membership functions. Of particular interest is the representation of continuous data for preventing loss of information. The non-parametric density estimation method applied here is a Parzen window estimation that can directly use continuous data without any categorization procedure. The effect of the new continuous data representation method on the final integrated result is evaluated by a validation procedure. To illustrate the proposed scheme, a case study from Jangheung, Korea for landslide hazard mapping is presented. Analysis of the results indicates that the proposed methodology considerably improves prediction capabilities, as compared with the case in traditional continuous data representation.

Uniformly Minimum Variance Unbiased Estimation for Distributions with Support Dependign on Two Parameters

  • Hong, Chong-Sun;Park, Hyun-Jip;Lee, Chong-Cheol
    • Journal of the Korean Statistical Society
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    • 제24권1호
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    • pp.45-64
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    • 1995
  • When a random sample is taken from a certain class of discrete and continuous distributions whose support depend on two parameters, we could find that there exists the complete and sufficient statistic for parameters which belong to a certain class, and fomulate the uniformly minimum variance unbiased estimator (UMVUE) of any estimable function. Some UMVUE's of parametric functions are illustrated for the class of the distribution. Especially, we find that the UMVUE of some estimable parametric function from the truncated normal distribution could be expressed by the version of the Mill's ratio.

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파라미터 불확실성을 갖는 이산시간 어핀 T-S 퍼지 시스템의 제어기 설계 (Controller Design for Discrete-Time Affine T-S Fuzzy System with Parametric Uncertainties)

  • 이상인;박진배;주영훈
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 하계학술대회 논문집 D
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    • pp.2516-2518
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    • 2004
  • This paper proposes a stability condition in discrete-time affine Takagi-Sugeno (T-S) fuzzy systems with parametric uncertainties and then, introduces the design method of a fuzzy-model-based controller which guarantees the stability. The analysis is based on Lyapunov functions that are continuous and piecewise quadratic. The search for a piecewise quadratic Lyapunov function can be represented in terms of linear matrix inequalities (LMIs).

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근사모델을 이용한 날개 평면형상 공력형상설계 방법 (Aerodynamic Shape Design Method for Wing Planform Using Metamodel)

  • 배효길;정소라
    • 항공우주시스템공학회지
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    • 제8권4호
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    • pp.18-23
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    • 2014
  • In preliminary design phase, the wing geometry of the civil aircraft was determined using the empirical equation and historical data. To make wing geometry more aerodynamically efficient, an aerodynamic shape optimization was conducted. For this purpose the parametric modeling, high fidelity CFD analysis and metamodel-based optimal design technique were adopted. The parametric modeling got the design process to achieve the improvement by generating the configuration outputs easily for the major design variables. The optimal design equations were formularized as the type of the multi-objective functions considering low/high speed and lift/drag coefficient. The optimal solution was explored with the help of the kriging metamodel and the desirability function, therefore the optimal wing planform was sought to be excellent at both low and high speed region. Additionally the optimal wing planform was validated that it was excellent not only at the specific AOA, but also all over the range of AOA.