• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2001년도 추계 학술대회논문집
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• pp.99-105
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• 2001

Flow computations have been conducted to study the impingement flowfield over the KSR-III flume deflector To validate Euler solver for the jet impingement flowfieid, the jet flow over a double wedge deflector have been calculated and showed reasonable agreement with experimental data. The transient flow behavior of flume over deflector have been investigated and the flume from the rocket nozzle proved to be getting out of the deflector safely and the thermal effect on the base region of rocket was not considerable.

• 한국융합학회논문지
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• 제11권8호
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• pp.159-163
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• 2020

본 연구에서는 트레일러의 디플렉터의 유무 및 그 형상들에 따른 주위의 유동해석을 하였다. 디플렉터가 없는 경우는 디플렉터가 있는 경우보다 컨테이너 뒤로 생기는 난류의 운동에너지도 더 넓은 영역에서 더 높은 운동 에너지가 발생하여 그 항력으로 인하여 차량의 주행성에 나쁜 영향을 미친다. 트레일러의 윈드 디플렉터가 없는 모델은 디플렉터가 있는 모델보다 트레일러 주변 유속이 불안정하고, 난류의 운동에너지도 많이 생겨서, 트레일러에 디플렉터를 설치하므로서 그 연비상승을 기대할 수 있다고 사료된다. 윈드 디플렉터 형상에 따른 트레일러 주위의 유동해석에 대한 연구결과를 적용함으로서, 본 연구가 미적인 융합에 적합된다고 보인다.

• 한국자동차공학회논문집
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• 제17권1호
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• pp.182-189
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• 2009

The noise from the sunroof can be divided into the low frequency buffeting noise and the high frequency turbulence noise generated when a car runs at the high driving speed. The wind deflector suppresses the buffeting noise generation by accelerating the vortex shedding from the front edge of sunroof opening, and guides the flow direction so that air can pass smoothly over the sunroof opening. To reduce the buffeting noise and the high frequency noise, it is very important to locate a deflector in a proper position depending on the driving speed and the sunroof opening width. The deflector's sectional shape also plays an important role in efficiently reducing the buffeting and high frequency noise. In this paper, we determined the optimum deflector's sectional shape and examined the flow characteristics behind a sunroof deflector through CFD analysis with changing the deflector height, the driving speed and the sunroof opening width. It is found that the deflector needs to be located in the higher location to control the buffeting noise by shedding the higher frequency vortices to accelerating vortices from the sunroof front edge. The deflector may act as a new noise source at the high driving speed, then it is desirable to put the deflector at the proper height to reduce the flow fluctuations and the noise generation. We also made a road test to verify CFD analysis results in this study.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.494-498
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• 2001

When supersonic jet impinges on wall from the nozzle, complex flow pattern appears such as Mach disc, expansion fan, and jet boundary. The numerical computation of this supersonic jet is important on flame deflecctor design for launch space especially. In this paper, we analyzed supersonic jet structure impinging on deflector wall using three dimensional steady and unsteady compressible equation and showed temperature and pressure distribution on the wall surface. As a result, some dominant factors of jet flows are discussed for conceptual design of flame deflector.

• 한국소음진동공학회논문집
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• 제26권1호
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• pp.13-19
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• 2016

The flow-excited Helmholtz resonance phenomenon was investigated numerically using Reynolds averaged Navier-Stokes approach. The fundamental cause of the Helmholtz resonance phenomenon is known as shedding of a single discrete vortex from orifice edge that travels during one period of the oscillation. In this study, serrated deflector, which is biomimetic design of the owl's feather, is used to split a single vortex into small vortices. Rectangular deflector and serrated deflector are compared with numerical results of pressure and streamline inside the cavity. Consequently, the serration breaks the shedding period of vortex core and eliminates the resonance. Also, it changes the flow pattern in according to the location of different serration height. By making inflows and outflows occur simultaneously in spanwise direction in the cavity, the period of Helmholtz resonance disappears. Comparing between rectangular deflector and serrated deflector, the serrated deflector can deal with the Helmholtz resonance more effectively.

• 한국생산제조학회지
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• 제23권2호
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• pp.138-144
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• 2014

This study investigates the air resistance due to deflector configurations of commonly used largetrucksat a driving speedof 80 km/h. Of the 6 models that are considered, the drag causedby the pressure on the front part of the trailer is largest for model 1. For model 1, the lift caused by the difference between the velocities of the upper and lower streams isgreatest amongall the models. Model 6 has the least resistance against the flow stream consideringthedrags and lifts of theflow models. Anoptimal design can be obtainedby investigating thesimulation analysis ofvarious deflector configurationsfor the upper part of largetrucks; this optimum deflector configuration will help reduce the air resistanceon large trucks.

• 한국음향학회지
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• 제37권5호
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• pp.285-291
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• 2018

본 연구에서는 차량에 장착되는 파노라마 썬루프 디플렉터의 각도에 따른 개구부 주변 유동 특성을 분석하고 공력소음에 미치는 영향을 확인하였다. 파노라마 썬루프 개방 후 주행 시 공력소음을 저감하기 위해 메쉬 디플렉터를 장착하는데, 후방향인 기존 메쉬 디플렉터 각도를 전방향으로 변경하였을 때 유동 변화와 공력소음 기여도를 분석하였다. 이를 위하여 CAT(Computer Aided Test)와 실차 풍동 평가를 진행하였으며, 전방경사형 디플렉터에서 기존 디플렉터 대비 원활한 유동의 흐름과 유동 방향의 상향으로 공력소음이 개선되는 것을 확인하였다. 전방경사형 디플렉터 적용 시 동등한 원가에서 공력소음을 개선할 수 있을 것으로 기대된다.

• 항공우주시스템공학회지
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• 제15권6호
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• pp.10-18
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• 2021

A flame deflector prevents a launch system from thermal damage by deflecting the exhaust flame of the launch vehicle. During the deflection of the flame, the flame deflector is subjected to a high-temperature and high-pressure flow, which results in thermal ablation damage at the surface. Predicting this ablation damage is an essential requirement to ensure a reliable design. This paper introduces a numerical method for predicting the ablation damage phenomena based on a one-way fluid-structure interaction (FSI) analysis. In the proposed procedure, the temperature and convective heat transfer coefficient of the exhaust flame are calculated using a fluid dynamics analysis, and then the ablation is calculated using a finite element analysis (FEA) based on the user-subroutine UMESHMOTION and Arbitrary Lagrangian-Eulerian (ALE) adaptive mesh technique in ABAQUS. The result of such an analysis was verified by comparison to the ablation test result for a flame deflector.

• 한국가시화정보학회지
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• 제19권3호
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• pp.46-53
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• 2021

In the present study, wind tunnel experiments were performed to reduce the drag of a paragliding helmet in the range of Reynolds numbers from 46,000 to 155,000. The drag force of the helmet model with dimples and deflectors installed was measured by varying the dimple depth and the slant angle of the deflector. The dimples were effective in reducing the drag at low Reynolds numbers, but no significant drag reduction was found in the Reynolds number range in which an actual paraglider flight takes place. On the other hand, the deflector installed tangentially to the side outline of the helmet showed an average drag reduction of 7% in the flight Reynolds number range of real paragliding. This was because the deflector shrunk the size of the wake region and moved the wake region downstream of the deflector.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.313-316
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• 2011

초음속 유동과 2상 유동이 공존하는 화염유도로 내 유동해석을 위한 사전 해석검증의 일환으로, 초음속 단상 노즐 플룸의 2차원 축대칭 해석과 물 분사가 포함된 3차원 2상 아음속 유동을 해석하였다. 단상초음속 노즐 플룸의 경우 충격파 셀 구조를 통해 물리적으로 위배되는 현상은 발견되지 않았다. 물분사가 포함된 3차원 2상 아음속 유동의 경우, 액적의 거동과 기화 과정을 정성적으로 볼 수 있었으며 물 분사시 고온공기의 냉각 모사가 가능함을 확인할 수 있었다. 이들 기초 검증 결과들은 추후 초음속 2상 물분사 플룸 유동에 적용되어 3차원 화염유도로 해석에 응용될 예정이다.