• Title/Summary/Keyword: Fan speed

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Labour of Love: Fan Labour, BTS, and South Korean Soft Power

  • Proctor, Jasmine
    • Asia Marketing Journal
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    • 제22권4호
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    • pp.79-101
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    • 2021
  • With the steady rise in global popularity of the Korean music group BTS, the South Korean government and surrounding industries have swiftly begun utilizing their image and international recognition for specific nation branding purposes. While K-pop soft power strategies are not novel to the South Korean state, what is new is the rapid speed at which BTS have become a beacon for South Korean culture, language, and symbolism in the international arena. However, few scholarly works have sought to investigate the role fans have played in this heightened position for the group as state representatives, with minimal research conducted into the work fans do within the framework of ARMY fan culture. This paper will thus aim to fill the gap in scholarship on ARMY as an organized labour network, focusing on the role fans play as labourers in online spaces that work to promote, disseminate, and cultivate wider recognition for BTS as artists. Through the conjunct engagement of a political economy framework and theories of participatory culture, this paper will explore the manner through which the free labour of ARMY, premised on affect, has constructed the fandom as active agents of soft power alongside BTS themselves.

Power-Space Functions in High Speed Railway Wireless Communications

  • Dong, Yunquan;Zhang, Chenshuang;Fan, Pingyi;Fan, Pingzhi
    • Journal of Communications and Networks
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    • 제17권3호
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    • pp.231-240
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    • 2015
  • To facilitate the base station planning in high speed railway communication systems, it is necessary to consider the functional relationships between the base station transmit power and space parameters such as train velocity and cell radius. Since these functions are able to present some inherent system properties determined by its spatial topology, they will be referred to as the power-space functions in this paper. In light of the fact that the line-of-sight path persists the most power of the received signal of each passing train, this paper considers the average transmission rate and bounds on power-space functions based on the additive white Gaussian noise channel (AWGN) model. As shown by Monte Carlo simulations, using AWGN channel instead of Rician channel introduces very small approximation errors, but a tractable mathematical framework and insightful results. Particularly, lower bounds and upper bounds on the average transmission rate, as well as transmit power as functions of train velocity and cell radius are presented in this paper. It is also proved that to maintain a fixed amount of service or a fixed average transmission rate, the transmit power of a base station needs to be increased exponentially, if the train velocity or cell radius is increased, respectively.

NSGA-II 를 통한 송풍기 블레이드의 다중목적함수 최적화 (Multi-Objective Optimization of a Fan Blade Using NSGA-II)

  • 이기상;김광용;압두스사마드
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2690-2695
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    • 2007
  • This work presents numerical optimization for design of a blade stacking line of a low speed axial flow fan with a fast and elitist Non-Dominated Sorting of Genetic Algorithm (NSGA-II) of multi-objective optimization using three-dimensional Navier-Stokes analysis. Reynolds-averaged Navier-Stokes (RANS) equations with ${\kappa}-{\varepsilon}$ turbulence model are discretized with finite volume approximations and solved on unstructured grids. Regression analysis is performed to get second order polynomial response which is used to generate Pareto optimal front with help of NSGA-II and local search strategy with weighted sum approach to refine the result obtained by NSGA-II to get better Pareto optimal front. Four geometric variables related to spanwise distributions of sweep and lean of blade stacking line are chosen as design variables to find higher performed fan blade. The performance is measured in terms of the objectives; total efficiency, total pressure and torque. Hence the motive of the optimization is to enhance total efficiency and total pressure and to reduce torque.

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횡방향 유속 변화에 따른 고압 가솔린 팬형 인젝터의 분무특성 (Spray Characteristics of High Pressure Fan Spray Injector with Various Crossflow Speed)

  • 최재문;문석수;배충식
    • 한국분무공학회지
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    • 제10권3호
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    • pp.38-44
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    • 2005
  • The direct injection into the cylinders has been regarded as a way of the reduction in fuel consumption and pollutant emissions. The spray produced from the injector of DIS(Direct Injection Spark Ignition) engine is of paramount importance in DISI engines. Fan-spray injector as well as swirl-spray injector was developed and utilized to the DISI engines. The interaction between air flow and fuel spray was investigated in a steady flow system embodied in a wind tunnel to simulate the variety of flow inside the cylinder of the DISI engineer. The direct Mie scattered images presented the macroscopic view of the liquid spray fields interacted with crossflow. Particle sizes of fuel droplets were measured with phase Doppler anemometer(PDA) system. A faster cross-flow field made SMD larger and $D_{10}$ smaller. The experiments show the interaction of air flow field and the fuel spray field of fan-spray. The results can be utilized to construct the data-base for the spray and fuel-air mixing mechanism as a function of the flow characteristics.

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유량에 따른 축류홴의 익단누설와류 및 후류 특성 (Flow Characteristics of Wake Flow with Relation to a Tip Leakage Vortex at Different Flow Rates in an Axial Flow Fan)

  • 김광용;장춘만
    • 대한기계학회논문집B
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    • 제29권3호
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    • pp.322-329
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    • 2005
  • The flow characteristics in the blade passage and in the wake region of a low speed axial flow fan have been investigated by experimental analysis using a rotating hot-wire sensor for design and off-design operating conditions. The results show that the tip leakage vortex is moved upstream when flow rate is decreased, thus disturbing the formation of wake flow near the rotor tip. The tip leakage vortex interfaces with blade pressure surface, and results in high velocity fluctuation near the pressure surface. From axial velocity distributions downstream of the fan rotor, large axial velocity decay near the rotor tip is observed at near stall condition, which results in large blockage compared to that at the design condition. Although the wake flow downstream of the rotor blade is clearly measured at all operating conditions, the trough of the high velocity fluctuation due to Karmann vortex street in the wake flow is mainly observed at a higher flow condition than the design flow rate.

Influence of Blade Row Distance on Performance and Flow Condition of Contra-Rotating Small-Sized Axial Fan

  • Shigemitsu, Toru;Fukutomi, Junichiro;Shimizu, Hiroki
    • International Journal of Fluid Machinery and Systems
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    • 제5권4호
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    • pp.161-167
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    • 2012
  • Small-sized axial fans are used as air coolers for electric equipment. There is a strong demand for higher power of fans according to the increase of quantity of heat from electric devices. Therefore, higher rotational speed design is conducted, although, it causes the deterioration of the efficiency and the increase of noise. Then, the adoption of contra-rotating rotors for small-sized fans is proposed for the improvement of the performance. In the case of contra-rotating rotors, blade row distance between the front and the rear rotors influences on the performance and the noise. Therefore, it is important to clarify the optimum blade row distance between front and rear rotors. The performance curves of the contra-rotating small-sized axial fan under the condition of different blade row distances are shown and the blade row interaction between the front and the rear rotors are discussed by the numerical results. Furthermore, the optimum blade row distance of the contra-rotating small-sized axial fan is considered.

네트워크형 지하 도로터널 분기부에서의 환기효율 향상방안에 대한 실험적 연구 (Experimental study of improvement of ventilation efficiency at intersection in network-form underground road tunnel)

  • 이호석;홍기혁;최창림;강명구;임재범;문홍표
    • 한국터널지하공간학회 논문집
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    • 제14권2호
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    • pp.107-116
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    • 2012
  • 네트워크형 도로터널 내 분기부 구조물과 제트팬에 의한 분기 환기효율 분석하고자 실제 도로터널을 1/45로 축소하여 실험을 수행하였다. 차량이 주행할 때 발생하는 교통관성력을 적용하기 위해 블로워 팬를 사용하여 축소모형 터널내 기류를 형성하였고, 터널의 국부적인 위치에서 속도를 측정하여 분기 효율을 연구하였다. 구조물의 특징으로 발생되는 환기 저감을 개선하기 위해 제트팬을 설치하여 터널 내 환기 효율을 최적화하였다.

Multi-Objective Shape Optimization of an Axial Fan Blade

  • Samad, Abdus;Lee, Ki-Sang;Kim, Kwang-Yong
    • International Journal of Air-Conditioning and Refrigeration
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    • 제16권1호
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    • pp.1-8
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    • 2008
  • Numerical optimization for design of a blade stacking line of a low speed axial flow fan with a fast and elitist Non-Dominated Sorting of Genetic Algorithm(NSGA-II) of multi-objective optimization using three-dimensional Navier-Stokes analysis is presented in this work. Reynolds-averaged Navier-Stokes(RANS) equations with ${\kappa}-{\varepsilon}$ turbulence model are discretized with finite volume approximations and solved on unstructured grids. Regression analysis is performed to get second order polynomial response which is used to generate Pareto optimal front with help of NSGA-II and local search strategy with weighted sum approach to refine the result obtained by NSGA-II to get better Pareto optimal front. Four geometric variables related to spanwise distributions of sweep and lean of blade stacking line are chosen as design variables to find higher performed fan blade. The performance is measured in terms of the objectives; total efficiency, total pressure and torque. Hence the motive of the optimization is to enhance total efficiency and total pressure and to reduce torque.

측정장치 압력손실과 면적평균 물리량 보정을 위한 다단 축류 팬과 압축기의 수치해석적 연구 (Numerical Investigation on Multi-stage Axial Fan and Compressor for Considering Pressure Losses by Instrumentation and Area-averaged Properties)

  • 최재호;김세미;이원석;최태우;김진욱
    • 한국수소및신에너지학회논문집
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    • 제29권4호
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    • pp.401-409
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    • 2018
  • A numerical investigation has been conducted to find the effects of pressure losses by struts and rakes, and averaging methods on the performance of a multi-stage axial fan and a multi-stage axial compressor. Struts and rakes which produce pressure losses are installed upstream of the aerodynamic inlet plane in the fan and the compressor rigs. Some of normal stator vanes are substituted with thick vanes with total pressure probes to measure total pressure between stages. Three-dimensional Reynolds-averaged Navier- Stokes equations with $k-{\omega}$ SST turbulence model were applied to analyze the pressure losses by the struts, inlet rakes, and thick instrumented vanes. The hexahedral grids were used to construct computational domain. Inlet pressure losses were evaluated for the compressor as a function of Mach number. The passage pressure losses due to the instrumented vanes were evaluated at the two speed lines in the fan. Total properties, such as pressure and temperature, were evaluated at the exit of the fan and the compressor with two different averaging methods which are area-averaging and mass-averaging, respectively.

덕트 팬의 동특성 연구 (Dynamic Characteristics of Ducted Fan: A Study)

  • 백상민;권재룡;이욱
    • 항공우주시스템공학회지
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    • 제11권6호
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    • pp.84-91
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    • 2017
  • 덕트 팬의 정지 비행시 동특성에 관한 연구를 수행하였다. 팬에 적용되는 블레이드에 대해서 단면 모델링을 수행하였으며, 로터 시스템의 구성요소들을 고려하여 해석 모델을 구축하였다. 로터의 회전수 및 피치각 조건에 따른 동특성 해석을 수행하였으며, 해석 결과 제안된 덕트 팬 시스템은 설계 운용범위 내에서 진동 증가와 같은 공탄성학적 불안정성이 적음을 확인하였다. 해석 절차의 검증을 위해 실제덕트 팬 회전 시험장치를 구성하였다. 기능 시험을 수행하여 덕트 팬 시험장치의 구성품간 거동 및 간섭 여부를 확인하였다. 동특성 시험을 위해 유압가진기를 사용하여 콜렉티브 가진을 하였으며, 비회전/회전시 블레이드의 고유진동수를 측정하였다. 시험 결과와 해석 결과의 비교를 통해 시험 장치와 해석 모델간의 상관관계가 잘 정립되어 있음을 확인하였다.