• 제목/요약/키워드: Leading Edge

검색결과 663건 처리시간 0.029초

입구 경계층 두께가 축류 압축기 내부 유동에 미치는 영향 (I) - 허브 코너 실속 및 익단 누설 유동 - (Effects of the Inlet Boundary Layer Thickness on the Flow in an Axial Compressor (I) - Hub Corner Stall and Tip Leakage Flow -)

  • 최민석;박준영;백제현
    • 대한기계학회논문집B
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    • 제29권8호
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    • pp.948-955
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    • 2005
  • A three-dimensional computation was conducted to understand effects of the inlet boundary layer thickness on the internal flow in a low-speed axial compressor operating at the design condition($\phi=85\%$) and near stall condition($\phi=65\%$). At the design condition, the flows in the axial compressor show, independent of the inlet boundary layer thickness, similar characteristics such as the pressure distribution, size of the hub comer-stall, tip leakage flow trajectory, limiting streamlines on the blade suction surface, etc. However, as the load is increased, the hub corner-stall grows to make a large separation region at the junction of the hub and suction surface for the inlet condition with thick boundary layers at the hub and casing. Moreover, the tip leakage flow is more vortical than that observed in case of the thin inlet boundary layer and has the critical point where the trajectory of the tip leakage flow is abruptly turned into the downstream. For the inlet condition with thin boundary layers, the hub corner-stall is diminished so it is indistinguishable from the wake. The tip leakage flow leans to the leading edge more than at the design condition but has no critical point. In addition to these, the severe reverse flow, induced by both boundary layer on the blade surface and the tip leakage flow, can be found to act as the blockage of flows near the casing, resulting in heavy loss.

소형 송풍기 소음의 음향학적 상사성에 관한 연구 (Acoustical Similarity for Small Cooling Fans Revisited)

  • 김용철;진성훈;이승배
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1995년도 춘계학술대회논문집; 전남대학교, 19 May 1995
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    • pp.196-201
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    • 1995
  • The broadband and discrete sources of sound in small cooling fans of propeller type and centrifugal type were investigated to understand the turbulent vortex structures from many bladed fans using ANSI test plenum for small air-moving devices (AMDs). The noise measurement method uses the plenum as a test apparatus to determine the acoustic source spectral density function at each operating conditions similar to real engineering applications based on acoustic similarity laws. The characteristics of fans including the head rise vs. volumetric flow rate performance were measured using a performance test facility. The sound power spectrum is decomposed into two non-dimensional functions: an acoustic source spectral distribution function F(St,.phi.) and an acoustic system response function G(He,.phi.) where St, He, and .phi. are the Strouhal number, the Helmholtz number, and the volumetric flow rate coefficient, respectively. The autospectra of radiated noise measurements for the fan operating at several volumetric flow rates,.phi., are analyzed using acoustical similarity. The rotating stall in the small propeller fan with a bell-mouth guided is mainly due to a leading edge separation. It creates a blockage in the passage and the reduction in the flow rate. The sound power levels with respect to the rotational speeds were measured to reveal the mechanisms of stall and/or surge for different loading conditions and geometries, for example, fans installed with a impinging plate. Lee and Meecham (1993) studied the effect of the large-scale motions like impinging normally on a flat plate using Large-Eddy Simulation(LES) and Lighthill's analogy.[ASME Winter Annual Meeting 1993, 93-WA/NCA-22]. The dipole and quadrupole sources in the fans tested are shown closely related to the vortex structures involved using cross-correlations of the hot-wire and microphone signals.

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초임계 CO2 발전용 파워터빈을 지지하는 틸팅패드 베어링의 열윤활 해석 및 패드 온도 측정 (Thermal Analysis and Temperature Measurement of Tilting Pad Bearings Supporting a Power Turbine for the Supercritical CO2 Cycle Application)

  • 이동현;김병옥;임형수
    • Tribology and Lubricants
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    • 제34권2호
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    • pp.43-48
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    • 2018
  • This paper presents the thermohydrodynamic analysis of tilting journal pad bearings supporting a power turbine rotor applied to a 250 kW super-critical $CO_2$ cycle. In the analysis, the generalized Reynolds equation and 3D energy equation are solved to predict oil film temperature and the 3D heat conduction equation is solved for pad temperature. The power turbine rotor is supported by two tilting pad bearings consisting of five pads with an oil supply block between the pads. Copper backing pads with higher thermal conductivity compared to steel backing pads are adopted to improve thermal management. The predicted maximum pad temperature is around $55^{\circ}C$ which is approximately $15^{\circ}C$ higher than oil supply temperature. In addition, the predicted minimum film thickness is 50 mm at a rotating speed of 5,000 rpm. These results indicate that there is no issue in the thermal behavior of the bearing. An operation test is performed with a power turbine module consisting of a power turbine, a reduction gear and a generator. Thermocouples are installed at the 75% position from the leading edge of the pad to monitor pad temperature. The power turbine uses compressed air at a temperature of $250^{\circ}C$ in its operation. The steady state pad temperatures measured in the test show good agreement with the predicted temperatures.

심포일을 갖는 가스 포일 저널 베어링의 성능 예측 (Performance Predictions of Gas Foil Journal Bearing with Shim Foils)

  • 황성호;문창국;이종성;김태호
    • Tribology and Lubricants
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    • 제34권3호
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    • pp.107-114
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    • 2018
  • This paper presents a computational model of a gas foil journal bearing with shim foils between the top foil and bumps, and predicts its static and dynamic performance. The analysis takes the previously developed simple elastic foundation model for the top foil-bump structure and advances it by adding foil models for the "shim foil" and "outer top foil." The outer top foil is installed between the (inner) top foil and bumps, and the shim foil is installed between the inner top foil and outer top foil. Both the inner and outer top foils have an arc length of $360^{\circ}$, but the arc length of the shim foil is shorter, which causes a ramp near its leading edge in the bearing clearance profile. The Reynolds equation for isothermal and isoviscous ideal gas solves the hydrodynamic pressure that develops within the bearing clearance with preloads due to the ramp. The centerline pressure and film thickness predictions show that the shim foil mitigates the peak pressure occurring at the loading direction, and broadens the positive pressure as well as minimum film thickness zones except for the shortest shim foil arc length of $180^{\circ}$. In general, the shim foil decreases the journal eccentricity, and increases the power loss, direct stiffness, and damping coefficients. As the shim foil arc length increases, the journal eccentricity decreases while the attitude angle, minimum film thickness, and direct stiffness/damping coefficients in the horizontal direction increase.

퍼지기반의 두뇌영상 영역분할 알고리듬 (Fuzzy-based Segmentation Algorithm for Brain Images)

  • 이효종
    • 대한전자공학회논문지TC
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    • 제46권12호
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    • pp.102-107
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    • 2009
  • 기술의 발달로 의료장비의 현대화가 이루어지고 PACS와 같은 시스템이 보편화되면서 디지털 의료영상처리 기술에 대한 관심이 높아지고 있다. 영역분할 기술은 디지털의료영상처리에서 첫 번째 단계로 필요한 전처리기술이다. 영역분할을 통하여 특정 부위가 종양, 부종, 파손 및 괴사세포와 같은 이상 현상을 나타내는 것을 조기에 발견할 수 있도록 해주고, 의사들이 적절한 처방을 내려줄 수 있도록 도와줄 수 있다. 특히 두뇌영상에서 백질, 회백질 및 CSF(cerebral spinal fluid)의 영역분할은 두뇌연구의 핵심기술이다. 이들 의료영상에서 기존의 윤곽선이나 영역 확장법은 애매한 경계선과 장기내의 물리적 특성이 비균질하여 영역분할의 실패율을 높게 한다. 퍼지기반의 영역분할 알고리듬은 불분명한 경계를 이루는 장기의 영역분할에 강하다고 알려져 있다. 본 연구에서는 자기공명영상이 강하게 나타내는 잡음에도 안정적인 퍼지기반의 영역분할 알고리듬을 제안하였다. 제안된 알고리듬은 이웃화소들을 군집시킬 때에 평균과 분산의 정보를 이용하여 최소한의 계산을 추가함으로써, 기존의 퍼지기반 영역분할 방법에 비하여 실패율이 대략 30% 이하로 낮은 것을 확인하였다.

Dynamic PIV를 이용한 난류경계층 내부 와구조 거동의 실험적 분석 (Experimental analysis of vortical structures in a turbulent layer using a dynamic PIV technique)

  • 최용석;이상준
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.193-196
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    • 2008
  • The vortical structures in a turbulent boundary layer (TBL) developed over a flat plate have been investigated experimentally. The flow conditions tested in this study were Re$_{\theta}$ = 3700, Re$_{\delta}$ = 11${\times}$105 and the shape factor H = 1.3. Instantaneous velocity fields in the streamwise-wall-normal planes were measured by using a dynamic PIV system. A trip-wire and sandpapers were placed behind the leading edge to promote the turbulent transition. 1000 velocity fields were obtained consecutively with a time interval of 1 millisecond. Streamwise u-velocity components were temporally averaged in the measuring plane. In addition, 2000 velocity fields were obtained randomly and ensemble-averaged to get the fully-developed turbulent characteristics. Profiles of the normalized u-component, turbulent intensities and Reynolds shear stress were evaluated. The structures of spanwise vortices were extracted from the instantaneous velocity fields by determining the swirling strength, ${\lambda}_{ci}$. The wall-normalized locations of vortices were temporally averaged in the measuring plane with respect to their rotational direction. The correlations between the temporally averaged u and the temporally averaged $y^+$ of vortices were evaluated. For the case of positive vortices, the correlation is not significant. However, the negative vortices show a strong negative correlation. The y-location of negative vortices tends to increase, as the averaged u decreases and vice versa. These findings indicate that the number of negative vortices in the outer layer increases during the outward bursting events.

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Investigation of surface pressures on CAARC tall building concerning effects of turbulence

  • Li, Yonggui;Yan, Jiahui;Chen, Xinzhong;Li, Qiusheng;Li, Yi
    • Wind and Structures
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    • 제31권4호
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    • pp.287-298
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    • 2020
  • This paper presents an experimental investigation on the surface pressures on the CAARC standard tall building model concerning the effects of freestream turbulence. Two groups of incidence turbulence are generated in the wind tunnel experiment. The first group has an approximately constant turbulence intensity of 10.3% but different turbulence integral scale varying from 0.141 m to 0.599 m or from 0.93 to 5.88 in terms of scale ratio (turbulence integral scale to building dimension). The second group presents similar turbulence integral scale but different turbulence intensity ranging from 7.2% to 13.5%. The experimental results show that the mean pressure coefficients on about half of the axial length of the side faces near the leading edge slightly decrease as the turbulence integral scale ratio that is larger than 4.25 increases, but respond markedly to the changes in turbulence intensity. The root-mean-square (RMS) and peak pressure coefficients depend on both turbulence integral scale and intensity. The RMS pressure coefficients increase with turbulence integral scale and intensity. As the turbulence integral scale increases from 0.141 m to 0.599 m, the mean peak pressure coefficient increases by 7%, 20% and 32% at most on the windward, side faces and leeward of the building model, respectively. As the turbulence intensity increases from 7.2% to 13.5%, the mean value of peak pressure coefficient increases by 47%, 69% and 23% at most on windward, side faces and leeward, respectively. The values of cross-correlations of fluctuating pressures increase as the turbulence integral scale increases, but decrease as turbulence intensity increases in most cases.

클라우드 서비스를 위한 고가용성 대용량 데이터 처리 아키텍쳐 (Implementation of Data processing of the High Availability for Software Architecture of the Cloud Computing)

  • 이병엽;박준호;유재수
    • 한국콘텐츠학회논문지
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    • 제13권2호
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    • pp.32-43
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    • 2013
  • 최근 많은 기관들로부터 클라우드 서비스가 향후 대세적인 IT서비스로의 확고한 기술로서 예견하고 있고, 실질적으로 IT를 리딩하는 많은 벤더 기업들을 주축으로 실질적인 클라우드 서비스를 제공 하고 있다. 따라서 클라우드 사용자는 서비스의 물리적인 위치나, 시스템 환경과 같은 부분들을 관여하지 않고, 스토리지 서비스, 데이터의 사용, 소프트웨어의 사용들을 제공하는 획기적인 서비스로 거듭나고 있다. 한편, 클라우드 컴퓨팅 기술들은 인프라스트럭처에서 요구되는 서비스의 수준, 다양한 시스템에서 요구되는 하드웨어적인 문제들을 벗어서 자유스럽게 원하는 만큼의 IT 리소스를 쉽게 사용할 수 있는 장점을 가지고 있지만, 고가용성 측면에서 반드시 기술적인 해결 방안을 모색하여야 한다. 따라서 본 논문 에서는 고가용성 측면에서의 클라우드 컴퓨팅을 위해 분산 파일 시스템이 갖추어야 할 사항들과 클라우드 컴퓨팅에서 활용 가능한 오픈소스 기반의 하둡 분산 파일 시스템, 메모리 데이터베이스 기술, 고가용성 데이터베이스 시스템을 소개하고 현재 클라우드 컴퓨팅 시장에서 활용되고 있는 분산 파일 시스템을 통한 분산처리 기술을 참고하여 고가용성 대용량 분산 데이터 처리 아키텍처를 클라우드 서비스 측면에서 구현하였다.

곤충비행에서 갑작스런 추력발생의 공기역학적 원인 Part 1: 와류 정지 및 와류 짝 현상 (The Aerodynamic Origin of Abrupt Thrust Generation in Insect Flight (Part 1: Vortex Staying and Vortex Pairing Phenomena))

  • 이정상;김진호;김종암
    • 한국항공우주학회지
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    • 제35권1호
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    • pp.1-9
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    • 2007
  • 검정금파리 날개의 “8자 운동”에 의한 공기역학적 힘의 발생에 관해 수치해석을 수행하였다. 날개운동은 자유류가 있는 tethered flight 실험에서 관찰된 결과에서 인용하였다. 해석결과 양력은 downstroke 중일 때 주로 발생하였고 추력은 upstroke 끝에서 갑작스럽게 발생하였다. 본 연구에서는 양력과 추력 발생의 이러한 특성을 후류에서의 와류구조와 에어포일 주위의 압력장을 통해 물리적으로 이해하고자 하였다. 결과적으로 양력발생은 유효받음각의 증가에 따른 앞전와류와 관계있었으며, 추력발생은 유동장 형태의 측면에서 와류 짝(vortex pairing)현상과 압력장 측면에서 와류정지 현상으로 설명할 수 있었다.

완공작 친환경 건축물 공모전의 평가기준 및 제출요구자료 특성 분석 - AIA COTE TOP 10 공모전과 녹색건축대전의 비교를 중심으로 - (Characteristics Analysis of Evaluation Measures and Submission Requirements of Sustainable Design Awards -Comparison between AIA COTE Top 10 and Korea Green Building Awards-)

  • 김진호;이도균
    • KIEAE Journal
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    • 제17권3호
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    • pp.59-67
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    • 2017
  • Purpose: As we are facing the global crisis from the climate change and energy depletion, urgent actions are needed to design a integrated sustainable building. This paper suggests that a sustainable design awards can stimulate for architects to bring the cutting-edge ideas into a realized building in comparison to green building certification system. AIA COTE Top 10 design awards, organized and run by AIA(American Institute of Architects) COTE(Committee on the Environment) from 1997, is analyzed as a case study. By researching the core of the AIA COTE Top 10 design awards system in terms of evaluation measures and submission requirements, meaningful suggestions were drawn to supplement Korea Green Building Awards system and to design and realize leading green buildings in Korea. Method: The comparison between AIA COTE Top 10 and Korea Green Building Design Awards was made in terms of evaluation measures, submission requirements, and green building certification systems. Result: This paper finally suggests the following three points in conclusion: 1) Set the standards of evaluation measures reflecting the three aspects(economy, environment, social) of sustainability, 2) Set the qualitative evaluation measures and corresponding submission requirements that can apply in the design awards in comparison to green building certification system, 3) Develop and balance submission requirements in response to evaluation measures to proceed systematic evaluation of the green buildings.