• Title/Summary/Keyword: computational calculation

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Multibody Dynamics in Arterial System

  • Shin Sang-Hoon;Park Young-Bae;Rhim Hye-Whon;Yoo Wan-Suk;Park Young-Jae;Park Dae-Hun
    • Journal of Mechanical Science and Technology
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    • v.19 no.spc1
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    • pp.343-349
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    • 2005
  • There are many things in common between hemodynamics in arterial systems and multibody dynamics in mechanical systems. Hemodynamics is concerned with the forces generated by the heart and the resulting motion of blood through the multi-branched vascular system. The conventional hemodynamics model has been intended to show the general behavior of the body arterial system with the frequency domain based linear model. The need for detailed models to analyze the local part like coronary arterial tree and cerebral arterial tree has been required recently. Non-linear analysis techniques are well-developed in multibody dynamics. In this paper, the studies of hemodynamics are summarized from the view of multibody dynamics. Computational algorithms of arterial tree analysis is derived, and proved by experiments on animals. The flow and pressure of each branch are calculated from the measured flow data at the ascending aorta. The simulated results of the carotid artery and the iliac artery show in good accordance with the measured results.

A Comparative Study of Interface Reconstruction Algorithms in The Molten Metal Flow (주조유동 시뮬레이션에서 자유경계면 추적 기법 비교 연구)

  • Choi, Young-Sim;Hong, Jun-Ho;Hwang, Ho-Young
    • Journal of Korea Foundry Society
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    • v.31 no.3
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    • pp.124-129
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    • 2011
  • We applied two numerical schemes to improve accuracy of the solution in the flow simulation of molten metal. One method is Piecewise Linear Interface Calculation (PLIC) method and the other is Donor-Acceptor (D-A) method. In the present work, we have tested simple problems to verify the module of the interface reconstruction algorithms. After validations, accuracy and efficiency of these two methods have compared by simulating various real products. On the numerical simulation of free surface flow, it is possible for PLIC method to track very accurately the interface between phases. PLIC method, however, has the weak point where a lot of computational time hangs, though it shows the more accurate interface reconstruction. Donor-Acceptor method has enough effectiveness in the macro observation of mold filling sequence though it shows the inferior accuracy.

Numerical Simulation of Unsteady CH$_4$/Air Jet Diffusion Flame (비정상 CH$_4$/공기 제트 확산화염에 관한 수치모사)

  • Lee, Chang-Eon;O, Chang-Bo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.8
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    • pp.1087-1096
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    • 2001
  • The dynamic structures of unsteady CH$_4$/Air jet diffusion flame with a flame-vortex interaction were numerically investigated. A timed-dependent, axisymmetric computational model and a low mach number approximation were employed in the present calculation. A two-step global reaction mechanism which considers 6 species, was used to calculate the reaction rates. The predicted results including the gravitational effect show that the large outer vortices and the small inner vortices can be well simulated without any additional disturbances near nozzle tip. It was found that the temperature and species concentrations have deviated values even for the same mixture fraction in the flame-vortex interaction region. It was also shown that the flame surface is not deformed by the inner vortex in upstream region, while in downstream region, the flame surface is compressed or stretched by the outer vortex roll-up. The present unsteady jet flame configuration accompanying a flame-vortex interaction is expected to give good implications for the unsteady structures of turbulent flames.

Improvement of Computational Efficiency of the Subspace Iteration Method for Large Finite Element Models (대형 유한요소 고유치 해석에서의 부공간 축차법 효율 개선)

  • Joo, Byung-Hyun;Lee, Byung-Chai
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.27 no.4
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    • pp.551-558
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    • 2003
  • An efficient and reliable subspace iteration algorithm using the block algorithm is proposed. The block algorithm is the method dividing eigenpairs into several blocks when a lot of eigenpairs are required. One of the key for the faster convergence is carefully selected initial vectors. As the initial vectors, the proposed method uses the modified Ritz vectors for guaranteering all the required eigenpairs and the quasi-static Ritz vectors for accelerating convergency of high frequency eigenvectors. Applying the quasi-static Ritz vectors, a shift is always required, and the proper shift based on the geometric average is proposed. To maximize efficiency, this paper estimates the proper number of blocks based on the theoretical amount of calculation in the subspace iteration. And it also considers the problems generated in the process of combining various algorithms and the solutions to the problems. Several numerical experiments show that the proposed subspace iteration algorithm is very efficient, reliable ,and accurate.

Vaporization of Hydrocarbon Fuel Droplet in High Pressure Environments (고압 환경하에서 탄화수소 연료 액적의 기화특성 연구)

  • Kim, Sung-Yup;Yoon, Woong-Sup
    • Proceedings of the KSME Conference
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    • 2003.11a
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    • pp.127-132
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    • 2003
  • A study of high-pressure n-heptane droplet vaporization is conducted with emphasis placed on equilibrium at vapor-liquid interface. General frame of previous rigorous model[1] is retained but tailored for flash equilibrium calculation of vapor-liquid interfacial thermodynamics. The model is based on complete time-dependent conservation equations with a full account of variable properties and vapor-liquid interfacial thermodynamics. The influences of high-pressure phenomena, including ambient gas solubility, thermodynamic non-ideality, and property variation on the droplet evaporation are investigated. The governing equations and associated moving interfacial boundary conditions are solved numerically using a implicit scheme with the preconditioning method and the dual time integration technique. And a parametric study of entire droplet vaporization history as a function of ambient pressure, temperature has been conducted. Some computational results are compared with Sato's experimental data for the validation of calculations. For low ambient temperatures, the droplet lifetime first increases with pressures, then decreases for high pressures. For higher ambient temperatures, the droplet lifetime increase with less amplitude than that of low ambient temperatures, which then decreases with more amplitude than that of low temperatures. The solubility of nitrogen can not be neglected in the high pressure and it becomes higher as the pressure goes up.

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Charge Transport Properties of Boron/Nitrogen Binary Doped Graphene Nanoribbons: An ab Initio Study

  • Kim, Seong Sik;Kim, Han Seul;Kim, Hyo Seok;Kim, Yong Hoon
    • Proceedings of the Korean Vacuum Society Conference
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    • 2014.02a
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    • pp.180.2-180.2
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    • 2014
  • Opening a bandgap by forming graphene nanoribbons (GNRs) and tailoring their properties via doping is a promising direction to achieve graphene-based advanced electronic devices. Applying a first-principles computational approach combining density functional theory (DFT) and DFT-based non-equilibrium Green's function (NEGF) calculation, we herein study the structural, electronic, and charge transport properties of boron-nitrogen binary edge doped GNRs and show that it can achieve novel doping effects that are absent for the single B or N doping. For the armchair GNRs, we find that the B-N edge co-doping almost perfectly recovers the conductance of pristine GNRs. For the zigzag GNRs, it is found to support spatially and energetically spin-polarized currents in the absence of magnetic electrodes or external gate fields: The spin-up (spin-down) currents along the B-N undoped edge and in the valence (conduction) band edge region. This may lead to a novel scheme of graphene band engineering and benefit the design of graphene-based spintronic devices.

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A Study on the Ku-band Corrugated Horn Antenna for Satellite Payload by using the Modal Expansion Method (모드 확장법을 이용한 Ku 밴드 위성탑재용 코루게이트 혼 안테나에 관한 연구)

  • 신응순;이영훈;윤영정;박한규
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.19 no.9
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    • pp.1802-1811
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    • 1994
  • In this paper, the corrugated horn antenna used in the reflector feed horn of satellite is analyzed using the modal expansion method. The modal expansion method is represented by the summations of modals at each point so the exact prediction of field and phase patterns can be obtained. The least number of iterations to compute field patterns is proposed. By using this number. calculation of accurate near and far field patterns without comsuming a lot of computational effort is available. Three kinds of corrugated horn antenna is designed to verify the method and experimented. The VSWR of designed frequency is from 1.04 to 1.1. The input impedance is nearly matched to $50\Omega$.

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An Improved frequency Synchronization Method Based on Autocorrelation function with Reduced Complexity (낮은 복잡도를 가지는 향상된 자기 상관 함수 기만의 주파수 동기화 기법)

  • Yang, Hyun;Jeong, Kwang-Soo;Lee, Kyeong-Il;Yi, Jae-Hoon;You, Young-Hwan
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.34 no.4C
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    • pp.424-429
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    • 2009
  • This paper suggests an autocorrelation function (AF) based carrier frequency offset (CFO) estimator based on a training sequence in flat fading channels. The proposed CFO estimator has the reduced computational burdens in the calculation of the AF when compared to AF-based conventional frequency estimators. The simulation results show that the proposed estimator achieves a better performance than the existing estimators. Furthermore, the performance of the proposed method has been observed to lie close to the Cramer-Rao lower bound (CRLB).

Performance Prediction of Centrifugal Compressors (원심 압축기의 성능 예측)

  • 오형우;정명균
    • Transactions of the Korean Society of Automotive Engineers
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    • v.5 no.2
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    • pp.136-148
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    • 1997
  • The present study has been carried out to develop a computational procedure for the analysis of the off-design performance in centrifugal compressors with vaneless diffusers by integrating empirical loss models and analytical equations. Losses in centrifugal compressors stem from a number of sources and their exact calculation is not yet possible. This study investigates several modeling schemes and shows that a fairly good prediction can be achieved by a proper selection of the most important flow parameters resulting form a meanline one-dimensional analysis. The performance maps for compressors are calculated and compared with measured performance maps. The off-design performance characteristics in terms of the pressure ratio vs. mass flow produced have generally correct forms. However, no universal means have been found to predict accurately the onset of surge. The prediction method developed through this study can serve as a tool to ensure good matching between parts and it can assist the understanding of the operational characteristics of general purpose centrifugal compressors.

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A Study on Low-Band-Shift with Integer Lifting for Effective Motion Estimation (효과적인 움직임 예측을 위한 정수형 리프팅 기반의 저대역 이동법에 관한 연구)

  • Baek, Jung-Eun;Jang, Sun-Bong;Shin, Jong-Hong;Jee, Inn-Ho
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.31 no.10C
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    • pp.948-955
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    • 2006
  • In this paper, we propose motion estimation and compensation using Low-Band-Shift(LBS) with Integer Lifting Shift property. To overcome shift-variant property on wavelet coefficients, the LBS was previously proposed. This method which is applied to reference frame in video coding technique has superior performance in terms of rate-distortion characteristic. However, this method needs more memory and computational complexity. For the enhancement of those disadvantages, we propose motion estimation using Low-Band-Shift with Integer Lifting. The Integer Lifting implementation gives us good efficiency of calculation and storage.