• 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.

• Advances in aircraft and spacecraft science
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• 제1권4호
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• pp.399-408
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• 2014

The flowfields inside a contour and a conical nozzle exhausting into a straight cylindrical supersonic diffuser are computed by solving numerically axisymmetric turbulent compressible Navier-Stokes equations for stagnation to ambient pressure ratios in the range 20 to 34. The diffuser inlet-to-nozzle throat area ratio and exit-to-throat area ratio are 21.77, and length-to-diameter ratio of the diffuser is 5. The flow characteristics of the conical and contour nozzle are compared with the help of velocity vector and Mach contour plots. The variations of Mach number along the centre line and wall of the conical nozzle, contour nozzle and the straight supersonic diffuser indicate the location of the shock and flow characteristics. The main aim of the present analysis is to delineate the flowfields of conical and contour nozzles operating under identical conditions and exhausting into a straight cylindrical supersonic diffuser.

• 반도체디스플레이기술학회지
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• 제21권4호
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• pp.163-167
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• 2022

In this paper, an optimization design method of a diffuser using Bernoulli's theorem was reviewed. The aspect ratio of the cylindrical diffuser chamber and the diameter ratio of the air inlet and outlet were used as design parameters. For the optimal design of the cylindrical diffuser chamber, the air flow inside the chamber was simulated using ANSYS while changing the aspect ratio of the chamber. In order to confirm the simulation results, the diffuser manufactured using the laser processing machine was measured. Through ANSYS simulation and measurement, it was found that the optimal design condition was when the aspect ratio (chamber height/radius) of the diffuser chamber was 1/2 and the diameter ratio of the air inlet and outlet was also 1/2.

• 한국군사과학기술학회지
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• 제7권4호
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• pp.138-145
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• 2004

Experimental study was conducted on cylindrical supersonic diffuser in order to investigate the effects of the ratios of diffuser area to nozzle throat area (Ad/At), diffuser area to nozzle exit area (Ad/Ae), nozzle exit area to its throat area (Ae/At), and diffuser length to its diameter (L/D), the free volume of vacuum chamber, and the relative distance between nozzle exit and diffuser inlet on the diffuser performance. The study showed that the minimum diffuser starting pressure (Po/Pa)st increased monotonically with increase in (Ad/At) as predicted by the normal shock and momentum theory models and the volume of vacuum chamber affected vacuum pressure level during diffuser operation at lower value of (Ad/Ae). The results of this investigation will be utilized in the design of real-scale high-altitude simulation test facility.

• 한국산업융합학회 논문집
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• 제25권4_2호
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• pp.637-644
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• 2022

In this study, the flow characteristics according to the shape of the vortex nozzle was studied by numerical analysis and the amount of microbubble generation was measured experimentally. The shape of the vortex nozzle is cylindrical, diffuser, and conical type. The axial fluid velocity in the induced tube gradually increased from the inlet to the outlet. In particular, the fluid velocity in the nozzle part increased rapidly. The velocity distribution of the fluid at the inlet of the induced tube showed that the flow rotates counterclockwise in the outer region and the inner center of the induced tube. At the outlet of the induced tube, the cylindrical and conical type showed rotational flow, and the diffuser type showed irregular turbulent flow. The dimensionless pressure ratio 𝜂 of the inner region of the induced tube was lower than that of the outer region. Also, 𝜂 near the outlet of the induced tube in cylindrical and conical type showed a similar tendency to the inlet area. At the outer region of inlet of induced tube, intense vorticity was observed on the wall and in lower region. At the inner region of inlet of induced tube, intense vorticity was observed on the inner wall of the induced tube and in the central region of the inlet of the induced tube. At the outlet of induced tube, in the case of the cylindrical and conical type, intense vorticity was observed near the inner wall, the diffuser type showed irregular strong vorticity inside the tube. The total number of bubbles measured was the most in the cylindrical type, and the microbubbles less than 50mm occurred the most in the conical type.

• Journal of the Korean Physical Society
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• 제73권11호
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• pp.1619-1624
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• 2018

Laser ablation may provide a minimally invasive palliative treatment for pancreatic cancer. The aim of the current study was to assess the feasibility of a 532-nm laser equipped with a cylindrical light diffuser for the treatment of pancreatic cancer. Monolayers of BxPC-3 human pancreatic cancer cell were exposed to 532 nm laser light. Power levels of 5 - 7 W were used to uniformly target the entire cell colonies for 60 and 120 seconds. The cells were incubated for 24 hours after treatment and viabilities were determined by using a MTT assay. Laser ablation was performed by using the cylindrical light diffuser on six pancreatic tumor tissues obtained from pancreatic cancer xenograft mouse models, which were exposed to the 532 nm light at 5W or 7W for 10 to 30 seconds. In the in vitro study, the survival rates of the pancreatic cancer cells were reduced by 6.6% to 98.9% after the treatment, and the survival rates were reduced by increasing laser power and/or irradiation time. In the pancreatic tumor tissues, a homogenous circular ablation zone was observed in all tumors and the ablation distance induced by the laser irradiation showed to be constant from the diffuser to all directions (standard deviation, 0.3 - 1.3 mm). Ablation distance and area increased with increasing laser power and/or irradiation time. The 532 nm laser effectively killed pancreatic cancer cells, and the cylindrical light diffuser was found to be suitable for laser ablation as it provided uniform ablation in pancreatic cancer.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.344-352
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• 2006

Evacuation performance, starting transient, and plume blowback at diffuser breakdown of a straight cylindrical supersonic exhaust diffuser with no externally supplied secondary flow are investigated. Pressure records in the transitional periods are measured by a small-scale cold-gas simulator. Flow-fields evolving in the diffuser-type ejector are solved by preconditioned Favre-averaged Navier-Stokes equations with a low-Reynolds number $k-{\varepsilon}$ turbulence model edited for turbulence compressibility effects. The present RANS method is properly validated with measured static wall pressure distributions and evacuation level at steady operation as well as the pressure records during the transition regime.

• 한국추진공학회지
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• 제13권5호
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• pp.21-28
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• 2009

본 연구는 초음속 축소형 디퓨저의 설계 및 시동 특성에 영향을 주는 변수를 파악하기 위하여 상온의 공기와 질소 가스를 사용하여 실험을 수행하였다. 1차 노즐의 목 면적의 변화, 1차 노즐 전단의 압력 변화, 디퓨저 길이와 직경의 비($L_d/D_d$) 그리고 디퓨저의 팽창부 유 무에 따른 디퓨저의 시동 특성을 알아보았다. 실험 결과 1차 노즐의 직경이 감소할수록 디퓨저 시동압력은 증가하였으며, 디퓨저의 예측 모델과 비교하여 90~98%의 장치 효율을 확인하였다. 또한 $L_d/D_d$가 8.4이상인 디퓨저와 팽창부의 유 무에 관계없이 디퓨저는 정상적으로 시동하였다. 본 실험 결과는 실물형 고고도 환경 모사 장치의 개발에 있어서 기초 자료로 활용될 것이다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.968-969
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• 2011

본 연구에서는 고고도 모사용 2차목 초음속 디퓨져의 특성을 알아보았고 작동 원리를 고찰하였다. STED의 경우 원통형 디퓨져보다 효율적으로 진공환경을 모사할 수 있는 것으로 알려져 있으므로 STED를 해석하였다. STED의 경우 디퓨져의 직경이 노즐 출구보다 크므로 노즐 배기는 디퓨져의 입구에 맞게 팽창되므로 그에 따라 배압이 감소함을 알 수 있었고 최초의 충격파가 보다 강도가 낮은 경사충격파로 바뀌면서 그에 따라 압력이 회복되어 디퓨져가 작동됨을 알 수 있었다.

• 항공우주기술
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• 제11권2호
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• pp.117-121
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• 2012

고공 환경 하에서 작동하는 우주발사체 상단 추진기관의 경우 지상에서 실제 작동 환경에 가까운 조건에서 연소시험을 수행하여 그 성능을 검증하게 된다. KSLV-I 상단 추진기관의 경우 원통형 디퓨저를 이용하여 고공환경 모사시험을 수행하였으며, 디퓨저의 설계 검증 및 시동특성을 확인하기 위해 축소형 디퓨저에 대한 비반응 유동시험 및 연소시험을 수행하였다. 본 논문에서는 축소형과 실물형 디퓨저에 대한 시험 결과를 제시하고 시동특성에 대해 분석하였다.