• 제어로봇시스템학회논문지
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• 제15권3호
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• pp.249-254
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• 2009

This paper studies the problem of pole placement by an LQ controller for system having two distinct real poles. Using the so-called Pole's Moving Range (PMR) drawn in the s-plane and relational equations between closed-loop system poles and weighting matrices, we calculate the state weighting matrix to move two distinct real poles to a pair of complex poles. By numerical examples, we show that the proposed method is applied to improve system performance.

• 한국경영과학회지
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• 제13권2호
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• pp.18-24
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• 1988

We consider sensitivity analysis sequencing problems, in which sequence of a finite set of expansion projects is sought to meet a deterministic demand projection in minimum discounted cost. In particular, by characterizing the underlying network structure, we find analytically the sensitivity range for a project cost such that the optimal sequencing policy remains unchanged for any value in the range. A numerical example is presented.

• Wind and Structures
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• 제17권6호
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• pp.647-670
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• 2013

The paper presents a numerical approach to study of fluid flow characteristics and to predict performance of wind turbines. The numerical model is based on Finite-volume method (FVM) discretization of unsteady Reynolds-averaged Navier-Stokes (URANS) equations. The movement of turbine blades is modeled using moving mesh technique. The turbulence is modeled using commonly used turbulence models: Renormalization Group (RNG) k-${\varepsilon}$ turbulence model and the standard k-${\varepsilon}$ and k-${\omega}$ turbulence models. The model is validated with the experimental data over a large range of tip-speed to wind ratio (TSR) and blade pitch angles. In order to demonstrate the use of numerical method as a tool for designing wind turbines, two dimensional (2-D) and three-dimensional (3-D) simulations are carried out to study the flow through a small scale Darrieus type H-rotor Vertical Axis Wind Turbine (VAWT). The flows predictions are used to determine the performance of the turbine. The turbine consists of 3-symmetrical NACA0022 blades. A number of simulations are performed for a range of approaching angles and wind speeds. This numerical study highlights the concerns with the self-starting capabilities of the present VAWT turbine. However results also indicate that self-starting capabilities of the turbine can be increased when the mounted angle of attack of the blades is increased. The 2-D simulations using the presented model can successfully be used at preliminary stage of turbine design to compare performance of the turbine for different design and operating parameters, whereas 3-D studies are preferred for the final design.

• 한국수자원학회논문집
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• 제46권12호
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• pp.1209-1220
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• 2013

본 연구에서는 내성천 하류 구간을 대상으로 검보정된 1차원 수치모형을 이용하여 흐름모의를 수행함으로써 추정된 구간 조도계수에 대해 분석하였다. 또한 실측 및 모의된 수리조건을 이용하여 향석 지점에서의 하상형태 예측을 수행하였으며 사립조도에 의한 흐름저항 계수 값을 고려하여 총 흐름저항 조도계수를 산정하였다. 수치모의에 의해 추정된 구간 조도계수와 사립조도 및 하상형태에 의한 흐름저항 계수를 추정한 결과 값을 상호 비교 분석하였으며 그 결과, 저수류 영역 흐름에서는 사립조도 및 하상형태에 의한 흐름저항 외에 식생, 만곡도, 사주 등의 기타 요인들에 의한 영향이 크게 반영되어 수치모의 상의 조도계수 값이 사립조도 및 하상형태에 의해 추정 가능한 조도계수 범위보다 크게 산정되는 것으로 나타났다. 그러나 $500m^3/s$ 이상의 천이구간 및 고수류 영역에서는 사립조도 및 하상형태 예측에 의한 조도계수 범위에 수치모의에 의해 검증된 Manning 조도계수가 포함되는 것으로 나타났다.

• 한국음향학회지
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• 제41권6호
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• pp.713-722
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• 2022

본 연구에서는 대상 원심팬 시스템에서 발생하는 유동 현상과 공력 음향 성능을 수치적/실험적으로 분석하고 다양한 수치 기법을 비교하여 평가하고자 하였다. 먼저 원심팬의 성능을 실험적으로 분석하기 위해 반무향실에서 음향 파워를 측정하였으며, 실험 결과를 통해 대상 원심팬 시스템에서 방사되는 소음 성능에 대한 유효 주파수 범위를 파악하고 이에 대한 수치 모사를 실시하였다. 수치적으로 유동 및 음향 파워를 분석하기 위해 Navier-Stokes 방정식과 Ffowcs Williams&Hawkings 방정식을 각각 유동장과 음향장의 지배방정식으로 사용하였으며, 음향장의 구현을 위해 가상의 음향 방사면을 설계하여 사용하였다. 고차 3차원 전산유체역학(Computational Fluid Dynamics, CFD)와 연계된 Hybrid-CAA 기법을 사용하여 모사한 음향 파워 레벨과 소음 실험을 통해 측정한 음향 파워 레벨의 비교를 통해 사용된 수치 기법의 정확도 및 수치적 특성을 평가하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.386-393
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• 2005

The objective of the present study is to develop a new type of the Ballistic range, called 'two-stage light gas gun'. A computational work has been performed to investigate the aerodynamics of a projectile which is launched from the two-stage light gas gun. A moving coordinate method for a multi-domain technique is employed to simulate unsteady projectile flows with a moving boundary. The effect of a virtual mass is added to the axisymmetric unsteady Euler equation systems. The computed results reasonably capture the major flow characteristics which are generated in launching the projectile supersonically, such as the interaction between the shock wave and the blast wave, the interaction between the vortical flow and the barrel shock, and the steady under-expanded jet. The present computational results properly predict the velocity, acceleration, and drag histories of the projectile.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회A
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• pp.467-472
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• 2007

A modern MEMS resonator is a micro-scale structure operated over a high frequency range. In order to predict its resonant behavior in a design process, High-frequency response analysis (Hi-FRA) is demanded. Algebraic substructuring (AS) is known as a fast numerical technique to construct an eigenspace for FR and frequency sweep (FS) algorithm efficiently solves the frequency response system projected on the eigenspace. However, the existing FS algorithm using AS is developed for low-FRA, say over the range 1Hz-2KHz. In this work, we extend the FS algorithm using AS for FRA over an arbitrary frequency range. Therefore, it can be efficiently applied to systems operated at a high frequency, say over the range 230MHz-250MHz. The success of the proposed method is demonstrated by Hi-FRA of a checkerboard resonator.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2010년도 춘계학술대회 논문집
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• pp.1011-1016
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• 2010

The noise emitted during train operation is generated with various reasons. It is known that the major noise generation is classified according to the ranges of train speed; that is, engine noise at lower speed range, rolling noise at medium speed range, and air-borne noise at higher speed range. These noises are transmitted in combined form with the noises generated from track components and under-carriage, etc. The rolling noise as a major noise at medium speed range is caused by the vibration occurred at wheel/rail interface. The vibration occurred at wheel/rail interface is transmitted to wheel and rail, and this vibration is emitted from wheel and rail as a noise. The object of this study is to investigate the effect of wheel damper of low noise wheel. In this study theoretical and experimental analysis is performed by numerical model calculations and impact test.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.1515-1517
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• 2008

The purposes of this study were to measure the ranges of motion in knee joint and during continuous passive motion(CPM) treatment and to computationally calculate joint angles at the knee joint dependent on the CPM machine design and its application. Four CPM machines and eleven candidates were recruited for this study. Experimental and numerical studies have been peformed to calculate the range-of-motion of CPM machines. From the experimental measurements, the average range of motions at the knee joint for the CPM machine #1, #2, #3, and #4 were lower than the manufactures suggested values due to improper alignments of the hip and knee joints to the CPM machines. Different design of CPM machine generated different outcomes of the ROM at the knee joints during CPM. The experiments and kinematic simulation in this study could be used to provide useful guidance in the treatment of CPM after joint surgery.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2005년도 동계학술발표대회 논문집
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• pp.63-68
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• 2005

In the present paper, the study on the optimal horizontal air jet velocity of a range hood system has been studied by three dimensional numerical simulation. It has been shown that the air jet of a range flood system generates coanda effect confining the contaminated (high temperature) air in a certain region while the jet pushes out more contaminated air into a room as the jet velocity increases. Therefore, the optimal jet velocity has been determined by the combination of the two mechanism.