• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2001년도 춘계학술대회 논문집
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• pp.63-68
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• 2001

In wide angle diffuser, the cross-sectional area increases so rapidly that separation can be avoided only by using boundary layer control. In this study, an experimental and numerical study is performed on performance of a diffuser with guide damper. A series of measurements were carried out to investigate the characteristics of diffuser for different divergence angle(${\phi}=7^{\circ}, \;10.5^{\circ}\;and\; 14^{\circ}$) of guide damper and angle of ${\phi}=10.5^{\circ}$ was through to be the best among three cases. Judging from the results, guide damper can be used as an effective means of improvement for diffuser performance.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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• pp.69-77
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• 1999

The aim of this paper is to understand the unsteady flow phenomena in a high speed centrifugal compressor channel diffuser. Instantaneous pressures are measured at six locations in the diffuser using fast-response pressure transducers. Instantaneous pressure ratio decomposition was applied to analyze the pressure signal. In vaneless space where impeller-vaned diffuser interaction is strong, aperiodic unsteadiness is high and periodic pressure waveforms by blade passing are not clear at low flow rates, especially near vane suction side. High aperiodic unsteadiness decreases downstream of diffuser. The blade-to-blade pressure wave does not disappear in surge flow condition. In surge there exist not only large scale periodic surge wave but also blade-to-blade pressure wave.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.442-447
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• 2008

A numerical analysis has been conducted to investigate and characterize the unsteadiness of flow structure and oscillatory vacuum pressure inside of a supersonic diffuser equipped to simulate the high-altitude rocket test on the ground. A physical model of concern includes a rocket motor, a vacuum chamber, and a diffuser, which have axisymmetric configurations, using nitrogen gas as a driving fluid. Emphasis is placed on investigating physical phenomena of very complex and oscillatory flow evolutions in the diffuser operating at very close to the starting condition, i.e. minimum starting condition, which is one of major important parameters in diffuser design points of view.

• Wind and Structures
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• 제32권1호
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• pp.47-53
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• 2021

This paper proposes a novel diffuser design for Diffuser Augmented Wind Turbines (DAWT) based on the blunt trailing edge airfoil AF300. Computational Fluid Dynamics (CFD) simulations are carried out to measure the performance of the AF300 diffuser against diffusers made with the shape of other high performance low wind speed airfoils. The results show that the proposed diffuser produces a greater air mass flow increase through the plane of the turbine than the other diffusers and it can be used to increase the performance of a horizontal axis wind turbine.

• 한국재료학회지
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• 제23권8호
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• pp.447-452
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• 2013

Recently, products that a have 3-dimensional(3D) micro structure have been in wide use. To fabricate these 3D micro structures, several methods, such as stereo lithography, reflow process, and diffuser lithography, have been used. However, these methods are either very complicated, have limitations in terms of patterns dimensions or need expensive components. To overcome these limitations, we fabricated various 3D micro structures in one step using a pair of diffusers that diffract the incident beam of UV light at wide angles. In the experiment, we used positive photoresist to coat the Si substrate. A pair of diffusers(ground glass diffuser, opal glass diffuser) with Gaussian and Lambertian scattering was placed above the photomask in the passage of UV light in the photolithography equipment. The incident rays of UV light diffracted twice at wider angles while passing through the diffusers. After exposure, the photoresist was developed fabricating the desired 3D micro structure. These micro structures were analyzed using FE-SEM and 3D-profiler data. As a result, this dual diffuser lithography(DDL) technique enabled us to fabricate various microstructures with different dimensions by just changing the combination of diffusers, making this technology an efficient alternative to other complex techniques.

• 한국전자파학회논문지
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• 제17권1호
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• pp.74-80
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• 2006

본 논문은 전자파 장해 및 복사 내성 측정의 대용 시험 시설로서 활용될 수 있는 전자파 잔향실의 전자기장 특성에 관한 연구이다. 잔향실 내에는 서로 다른 두 주파수 대역에서도 사용 가능한 이중 대역 확산기(diffuser)가 적용되었고, 이중 대역 확산기는 서로 다른 단일 대 역 Schroeder 방식의 QRD(Quadratic Residue Diffuser)로 합성되었다. 잔향실 내부의 전자기장 분포 해석을 위해서는 FDTD(Finite-Difference Time-Domain) 수치 해석 방식이 이용되었다. 잔향실에 사용된 이중 대역 확산기는 단일 대역 확산기에 비해 시험할 수 있는 주파수 대역 확장 뿐 아니라, 잔향실의 전자기장 균일도, 편파 특성, 전력 효율 및 공차 등의 성능을 향상시켰다. 따라서 이중 대역 확산기를 사용한 잔향실이 단일 대역 확산기를 사용한 잔향실보다 효율적인 시험시설로서 활용될 수 있음을 확인하였다.

• 대한기계학회논문집B
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• 제40권2호
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• pp.93-102
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• 2016

본 연구에서는 고고도의 저압 환경을 모사하기 위한 CBD(Center Body Diffuser)의 시동특성에 대한 실험적 연구를 수행하였다. Center Body Diffuser의 형상을 다양하게 구성할 수 있도록 실험 장치를 설계/제작하여, 상온 유동 실험을 통해 CBD 형상에 따른 저압환경 구현 성능과 시동 특성을 관찰하였다. 실험 결과 센터바디의 수축각이 약 15도 일 때 시동압력이 가장 낮은 것을 확인하였다. 또한 디퓨저 입구부 길이($L_d/D_d$)가 감소할수록, 확산부 길이($L_s$)가 증가할수록 시동특성이 크게 향상되었다. 또한 디퓨저 입구부 길이($L_d/D_d$) 변화만을 통해 진공 챔버 압력을 조절할 수 있는 CBD만의 설비적 장점을 확인하였다.

• 대한전자공학회논문지TC
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• 제45권8호
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• pp.121-127
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• 2008

본 논문은 원통형 확산기를 사용한 전자파 잔향실내의 전기장 분포에 관하여 다루었다. $1{\sim}3$ GHz 주파수 대역의 QRD(Quadratic Residue Diffuser)와 원통형 확산기(Cylindrical Diffuser)를 설계 후 각각의 전기장 분포 특성을 비교하였다. 전기장 분포 특성 및 전기장 균일도를 조사하기 위해 FDTD(Finite-Difference Time-Domain) 수치 해석 방법을 사용하였으며, 2 GHz에서 수치해석 결과 원통형 확산기를 사용하였을 경우 기존의 QRD를 사용한 경우에 비하여 표준편차와 공차는 각각 0.11 dB, 0.43 dB 개선되었고, 전기장 세기는 QRD의 36.6 dBmV/m보다 높은 43.2 dBmV/m로 나타났으며, 편파 특성면에서도 QRD보다 개선되었음을 확인 할 수 있었다. 따라서 원통형 확산기를 사용한 전자파 잔향실이 소형 전자기기의 전자파 장해 및 복사 내성 측정을 위한 대용시험 시설로 사용될 수 있음을 확인하였다.

• International Journal of Fluid Machinery and Systems
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• 제2권1호
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• pp.31-39
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• 2009

The flow instability in a low specific speed mixed-flow pump, having a positive slope of head-flow characteristics was investigated. Based on the static pressure measurements, it was found that a rotating stall in the vaned diffuser occurs at about 65% flow rate of best efficiency point (BEP). A dynamic Particle Image Velocimetry (DPIV) measurement and the numerical simulations were conducted in order to investigate the flow fields. As a result, the diffuser rotating stall was simulated even by Computational Fluid Dynamics (CFD) and the calculated periodic flow patterns agree well with the measured ones by DPIV. It is clarified that a periodical large scaled backflow, generated at the leading edge of the suction surface of the diffuser vane, causes the instability. Furthermore, the growth of the strong vortex at the leading edge of the diffuser vane induces the strong backflow from the diffuser outlet to the inlet. The scale of one stall cell is covered over four-passages in total thirteen vane-passages.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 1998년도 유체기계 연구개발 발표회 논문집
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• pp.217-222
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• 1998

CSCM upwind flux difference splitting compressible Navier-Stokes method has been used to predict the transonic flows in centrifugal compressor diffuser. The modified cyclic TDMA and the mass flux boundary conditions were used as boundary conditions of the diffuser analysis. With the mass flux boundary condition and the $130{\times}80{\times}40$ grid, the compressible upwind Navier-Stokes method predicted the transonic diffuser flowfield successfully. Plow changes in the impeller exit region due to the strong interaction between impeller exit and vaned diffuser, broad flow separation on the suction surface near hub and shroud was observed from the results of the mass flow rates 6.0 and 6.2kg/s at 27000 rpm. The static pressure increased and the total pressure decreased through the flow passage of the channel diffuser, which were predicted better from the three-dimensional analysis than from the two-dimensional analysis due to the strong effect of the three-dimensional flow. The mass averaged loss coefficients and pressure coefficients were also studied.