• 제목/요약/키워드: Mean low flow

검색결과 450건 처리시간 0.025초

2차원저천단구조물(LCS)의 주변에서 불규칙파동장의 변동특성 (Variation Characteristics of Irregular Wave Fields around 2-Dimensional Low-Crested-Breakwater)

  • 이광호;최군호;이준형;정욱진;김도삼
    • 한국해안·해양공학회논문집
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    • 제31권6호
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    • pp.356-367
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    • 2019
  • 본 연구는 olaFlow 모델에 의한 혼상류수치해석법을 적용하여 저천단구조물에 의한 불규칙파랑의 변동특성을 수치적으로 검토한다. 목표스펙트럼에 의한 불규칙파형과 측정된 불규칙파형과의 비교 및 이로부터 산정된 두 주파수스펙트럼의 비교로부터 olaFlow의 타당성을 검증하고, 2차원저천단구조물에 의한 불규칙파의 주파수스펙트럼의 변동, 파전달율, Hrms의 공간분포, 평균유속과 평균난류운동에너지의 공간분포 등을 수치적으로 검토한다. 이로부터 LCS 외해측의 전면에서 시계방향의 해빈류와 반시계방향의 순환류셀이 형성되고, 내해측의 정수면 근방에서 항내로 향하는 강한 일방향흐름이 발생되는 등의 중요한 결과를 얻을 수 있었다.

직사각형 단면을 갖는 $90^{\circ}C$ 급곡관 내의 3차원 난류유동에 관한 실험적 연구 (Experimental Study of Three-Dimensional Turbulent Flow in a $90^{\circ}C$ Rectanglar Cross Sectional Strongly Curved Duct)

  • 맹주성;류명석;양시영;장용준
    • 대한기계학회논문집
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    • 제15권1호
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    • pp.262-273
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    • 1991
  • 본 연구에서는 벽면에서의 압력은 압력측정 정치를 제작하여 측정하였으며 평 균유동 및 난류량들은 열선 유속계(hot wire system)을 사용하여 측정하였다.

가스 및 분무화염의 연소소음 특성에 관한 실험연구 (Combustion Noise Characteristics in Gas and Liquid Flames)

  • 김호석;백민수;오상헌
    • Journal of Advanced Marine Engineering and Technology
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    • 제18권1호
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    • pp.81-91
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    • 1994
  • Combustion noise involved with chemical heat release and turbulent process in turbopropulsion systems, gasturbine, industrial furnaces and internal engines is indeed noisy. The experimental study reported in this paper is made to identify a dominant combustion noise in jet flames. Gaseous propane and kerosene fuel have been used with air as the oxidizer in a different jet combustion systems. Combustion and aerodynamic noise are studied through far field sound pressure measurements in an anechoic chamber. And also mean temperature and velocities and turbulent intensities of both isothermal and reacting flow fields were measured. It is shown that axial mean velocity of reacting flow fields is higher about 1 to 3m/sec than that of cold flow in a gaseous combustor. As the gaseous fuel flow rate increases, the acoustic power increases. But the sound pressure level for the spray flame decreases with increasing equivalence ratio. The influence of temperature in the combustion fields due to chemical heat release has been observed to be a dominant noise source in the spray flame. The spectra of combustion noise in gaseous propane and kerosene jet flame show a predominantly low frequency and a broadband nature as compared with the noise characteristics in an isothermal air jet.

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씨로코팬의 유동특성에 관한 연구 (A Study on the Flow Characteristics of Sirocco fan)

  • 이덕구;김건일;정한별;설재림;이행남;박길문
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2005년도 전기학술대회논문집
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    • pp.200-204
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    • 2005
  • The sirocco fan is used to get low noise, and it has been applied to a lot of industry field like the heat engine, the fluid instrument power plant, the food industry, environment industry etc... because there are not any problem even it is mixed with a any kind of liquid, gas, and solid. The flow characteristics in sirocco fan are investigated by PIV. The experiment using PIV measurement for Test section's flow characteristics acquired velocity distribution, .Condition : when sirocco fan in automobile air controller maximum 1450RPM, and a revolution is a variation (1)950RPM, (2)1100RPM, (3)1250RPM. The agreement a experiment shows the validity of this study and the results of this study would be useful to the engineers who design for the flow systems for heating, ventilation and air conditioning.

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PIV와 CFD에 의한 Ejector내의 유동특성 연구 (A Study on the Flow Characteristics in Ejector by PIV and CFD)

  • 박지만;이행남;박길문;이덕구;설재림
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.723-728
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    • 2003
  • The Ejector is used to get low pressure, and it has been applied to a lot of industry field like the heat engine, the fluid instrument power plant, the food industry, environment industry etc... because there are not any problem even it is mixed with a any kind of liquid, gas, and solid. The flow characteristics in ejector are investigated by PIV and CFD. The experiment using PIV measurement for mixing pipe's flow characteristics acquired velocity distribution, kinetic energy distribution, and whirlpool . (Condition : when mixing pipe's diameter ratio is 1:1.9, and the flux is $Q_{1}=1.136{\imath}/s$, $Q_{2}=1.706{\imath}/s$, $Q_{3}=2.276{\imath}/s$. Based on the PIV and the CFD results, the flow characteristics in ejector are discussed, and it shows the validity of this study.

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IN-CYLINDER FLOW ANALYSIS USING WAVELET ANALYSIS

  • Park, D.;Sullivan, P.E.;Wallace, J.S.
    • International Journal of Automotive Technology
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    • 제7권3호
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    • pp.289-294
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    • 2006
  • Better fundamental understanding of the interactions between the in-cylinder flows and combustion process is an important requirement for further improvement in the fuel economy and emissions of internal combustion(IC) engines. Flow near a spark plug at the time of ignition plays an important role for early flame kernel development(EFKD). Velocity data measurements in this study were made with a two-component laser Doppler velocimetry(LDV) near a spark plug in a single cylinder optical spark ignition(SI) engine with a heart-shaped combustion chamber. LDV velocity data were collected on an individual cycle basis under wide-open motored conditions with an engine speed of 1,000rpm. This study examines and compares the flow fields as interpreted through ensemble, cyclic and discrete wavelet transformation(DWT) analysis. The energy distributions in the non-stationary engine flows are also investigated over crank angle phase and frequency through continuous wavelet transformation(CWT) for a position near a spark plug. Wavelet analysis is appropriate for analyzing the flow fields in engines because it gives information about the transient events in a time and frequency plane. The results of CWT analysis are provided and compared with the mean flows of DWT first decomposition level for all cycles at a position. Low frequency high energy found with CWT corresponds well with the peak locations of the mean velocity. The high frequency flows caused by the intake jet gradually decay as the piston approaches the bottom dead center(BDC).

저 레이놀즈 수 영역에서 날갯짓 비행체 공력 모델의 실험적 검증 (Experimental Validation of Ornithopter Aerodynamic Model in Low Reynolds Number Regime)

  • 이준성;김대관;한재흥
    • 한국항공우주학회지
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    • 제38권7호
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    • pp.647-654
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    • 2010
  • 본 연구에서는 날갯짓 비행체 날개의 유체-구조 연계를 고려한 설계나 날갯짓 비행체의 비행 동역학 및 제어 시뮬레이션에 적용 가능한 효율적인 공력모델을 제안하고, 풍동 실험을 통해 공력모델의 특성을 검증하고자 한다. 날갯짓 비행체는 저 레이놀즈 수 영역의 비정상 유동장의 지배를 받기 때문에, 이 영역에서 날개 운동에 따른 공력을 효과적으로 측정할 수 있도록 풍동실험장치를 설계 및 개발하였다. 본 연구의 실험장치 특성상 힘을 측정하는 2축-로드셀은 비관성계에 있기 때문에, 순수한 날개의 공력을 측정하기 위해서는 관성력을 보정해주어야 하며, 이에 대한 방법론을 수립하였다. 최종적으로 유동속도, 날개의 운동 주파수 및 고정 받음각에 따라 날개에 작용하는 양력 및 항력의 평균값 및 평균 제곱근 값을 비교함으로서 실험결과와 공력모델의 특성을 비교 검증하였다.

Systematic influence of different building spacing, height and layout on mean wind and turbulent characteristics within and over urban building arrays

  • Jiang, Dehai;Jiang, Weimei;Liu, Hongnian;Sun, Jianning
    • Wind and Structures
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    • 제11권4호
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    • pp.275-289
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    • 2008
  • Large eddy simulations have been performed within and over different types of urban building arrays. This paper adopted three dimensionless parameters, building frontal area density (${\lambda}_f$) the variation degree of building height (${\sigma}_h$), and the staggered degree of building range ($r_s$), to study the systematic influence of building spacing, height and layout on wind and turbulent characteristics. The following results have been achieved: (1) As ${\lambda}_f$ decrease from 0.25 to 0.18, the mean flow patterns transfer from "skimming" flow to "wake interference" flow, and as ${\lambda}_f$ decrease from 0.06 to 0.04, the mean flow patterns transfer from "wake interference" flow to "isolated roughness" flow. With increasing ${\lambda}_f$, wind velocity within arrays increases, and the vortexes in front of low buildings would break, even disappear, whereas the vortexes in front of tall buildings would strengthen and expand. Tall buildings have greater disturbance on wind than low buildings do. (2) All the wind velocity profiles and the upstream profile converge at the height of 2.5H approximately. The decay of wind velocity within the building canopy was in positive correlation with ${\lambda}_f$ and $r_s$. If the height of building arrays is variable, Macdonald's wind velocity model should be modified through introducing ${\sigma}_h$, because wind velocity decreases at the upper layers of the canopy and increases at the lower layers of the canopy. (3) The maximum of turbulence kinetic energy (TKE) always locates at 1.2 times as high as the buildings. TKE within the canopy decreases with increasing ${\lambda}_f$ and $r_s$ but the maximum of TKE are very close though ${\sigma}_h$ varies. (4) Wind velocity profile follows the logarithmic law approximately above the building canopy. The Zero-plane displacement $z_d$ heighten with increasing ${\lambda}_f$, whereas the maximum of and Roughness length $z_0$ occurs when ${\lambda}_f$ is about 0.14. $z_d$ and $z_0$ heighten linearly with ${\sigma}_h$ and $r_s$, If ${\sigma}_h$ is large enough, $z_d$ may become higher than the average height of buildings.

가압식 오실로메트릭 측정법에서 정확한 평균 동맥압 측정을 위한 노이즈 제거 알고리즘 (Noise Removal Algorithm for Accurate Mean Arterial Pressure Measurement in Pressurized Oscillometric Method)

  • 조인희;임정현;김영길
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2018년도 춘계학술대회
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    • pp.184-187
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    • 2018
  • 뇌경색의 예방 및 치료에 있어서 가장 중요한 요소는 대뇌 혈류량을 증가시키는 것이다. 대뇌 혈류를 증가시키는 방법으로는 기본적으로 약물에 의한 방법과 수술 또는 동맥 내에 의료 기구를 직접 삽입하는 침습적인 시술(NeuroFloTM) 등이 있다. 본 논문에서 제안하는 비 침습적인 대뇌 혈류 증가 장치는 합병증 유발 확률이 적고, 환자의 혈압 상태에 따라 치료 수준을 정할 수 있으므로 환자의 부담을 덜어줄 수 있다. 이러한 비 침습적인 대뇌 혈류 증가 장치 구현에 있어, 환자에게 알맞은 치료 수준을 제공하기 위한 정확한 평균 동맥압 값을 측정하는 것이 중요하다. 따라서 노이즈를 제거하기 위해 아날로그 필터 및 디지털 필터를 사용하였고, 피크 값 검출을 위한 알고리즘, 펌프제어 알고리즘 등을 사용하였다.

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A Novel Technoque for Characterization of Membranes

  • Webber, Ronald;Jena, Akshaya;Gupta, Krishna
    • 한국막학회:학술대회논문집
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    • 한국막학회 2001년도 제14회 심포지엄 : 제2회 분리막 표준화(The 2nd Standardization of Membranes)
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    • pp.39-50
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    • 2001
  • The performance of membranes is governed their pore struture. Pore structures of porous materials can be determined by a number of techniques. However, The novel technique, capillary folw porometry has a number of advantages. In this technique, the sample is brought in contact with a liquid that fills the pores in the membrane spontaneously. Gas under pressure is used to force the liquid from the pores and increase gas flow. Gas flow rate measured as a function of gas pressure in wet and dry samples yield data on the largest pore size, the mean flow pore size, flow distribution and permeability. Pore characteristics of a number of membranes were measured using this technique. This technique did not require the use of any toxic material and the pressure employed was low. Capillary flow porometry is a suitable technique for measurement of the pore structure of many membranes.

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