• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.634-643
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• 2004

In this paper are presented a concept of a new supersonic air inlet, which is designated a Multi-Row Disk (MRD) inlet, aiming at performance improvement under off-design conditions, and results of wind tunnel tests examined performance characteristics of the MRD inlet. The MRD inlet is frequently called ‘a skeleton inlet’ because of its appearance. The performance of a conventional axisymmetric inlet with a solid center body (spike) deteriorates under off-design Mach number conditions. It is due to the fact that total pressure recovery (TPR) governed by the throat area of inlet and mass capture ratio (MCR) governed by an incidence position of an oblique shock from the spike tip into the cowl can not be controlled independently in such air inlet. The MRD inlet has the spike that is composed of a tip cone and several disks arranged downstream of it, based on the experimental fact that several deep cavities on a conical surface have little negative effect on the boundary layer growth. The overall spike length of the MRD inlet is adjustable to the given flight speed by changing space between disks so that a spillage flow can be controlled independently from controlling the throat area. It could be made clear from the result of wind tunnel tests that the MRD inlet improves TPR by 10% compared with a conventional inlet with a solid spike under off-design conditions.

• 대한조선학회논문집
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• 제56권3호
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• pp.281-289
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• 2019

In order to investigate the influence of thru holes near leading edge of model propeller on cavitation behavior, a model propeller with thru holes was manufactured and tested at Large Cavitation Tunnel (LCT). The pressure distribution around the thru hole on propeller blade was numerically calculated to help understand the local flow characteristics related to cavitation behavior. The model propeller is a five bladed propeller which has 2 blades with thru holes and 3 blades with smooth surface. The cavitation observation tests were conducted at angles of $0^{\circ}$ & $6^{\circ}$ using an inclined-shaft dynamometer in LCT. There are big difference on the suction side cavitation behavior each other due to the existence of thru hole. While the blades with thou holes start generation of the sheet cavitation from the leading edge on the suction side, the blades with smooth surface generate the cloud cavitation from the mid-chord. Cavitation on the blades with thru holes shows more similar behavior to those of the full-scale propeller of which the pipe line for air injection is closed. The numerical analysis result shows that the sharp pressure drop occurs around thru holes on the blade. Consequently, the thru hole around leading edge stimulates the cavitation occurrence and stabilizes the cavitation behavior. Based on these results, the effect of thru holes on propeller cavitation behavior behind a model ship should be studied in the future.

• 한국터널지하공간학회 논문집
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• 제17권2호
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• pp.153-166
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• 2015

일반적인 장대 철도터널에 비해 해저터널은 환기 및 방재를 위한 별도의 연직갱 또는 경사갱 설치에 공간상 많은 제약을 받게 되므로, 인공섬을 건설하여 환기를 수행할 필요가 있다. 그러나, 인공섬 설치에는 시공상의 문제 뿐만 아니라 건설비용이 증가하게 되므로, 인공섬 설치를 최소화하여 환기구간 거리를 늘려야 한다. 이에 따른 환기거리의 증가시, 누풍에 의한 신선공기 공급량이 커지게 된다. 공급풍량이 과대해지면, 구조물 한계에 의해 설치가능한 덕트직경이 제한적이므로, 팬 정압 및 동력도 상당히 증가하게 된다. 따라서, 초장대 해저터널을 건설하기 위해서는 이러한 현실적인 문제를 극복하고, 시공중 터널내 환경을 쾌적한 상태로 유지할 수 있는 기술력이 필요하다. 본 논문에서는 이러한 초장대 해저터널에 적합한 공사중 환기 방식을 개발하기 위한 기본연구로써, 국내외의 공사중 환기용량 산정방법 비교를 통해, 스위스의 SIA 196 코드가 초장대 해저터널계획에 적합함을 확인하였다. 또한, 덕트 접속부의 누출에 관한 실험을 통해, 국내의 덕트 접속방식은 100 m당 누풍율이 1.5~3.0% 사이임을 확인하였다. S등급 덕트의 경우 환기가능거리가 10.2 km 이므로, 덕트의 접속방법을 개선한다면, 환기가능거리는 더 길어질 수 있다. 따라서, 공사중 덕트의 누풍개선이 초장대 해저터널의 공사중 환기의 주요 이슈임을 확인하였다.

• 대한기계학회논문집B
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• 제20권12호
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• pp.3980-3990
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• 1996

When a moist air is rapidly expanded in a supersonic nozzle, nonequilibrium condensation occurs at a supersaturation state. Condensation shock wave appears in the nozzle flow if the releasing latent heat due to condensation goes beyond a critical value. It has been known that self-excited oscillations of the condensation shock wave generate in an air or a steam nozzle flow with a large humidity. In the present study, the passive control technique using porous wall with a cavity underneath was applied to the condensation shock wave. The effects of the passive control on the steady and self-excited condensation shock waves were experimentally investigated by Schlieren visualization and static pressure measurements. The result shows that the present passive control is a useful technique to suppress the self-excited oscillations of condensation shock wave.

• Wind and Structures
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• 제15권6호
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• pp.481-494
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• 2012

The greenhouse type metal structures are increasingly used in modern construction of livestock farms because they are less laborious to construct and they provide a more favorable microclimate for the growth of animals compared to conventional livestock structures. A key stress factor for metal structures is the wind. The external pressure coefficient ($c_{pe}$) is used for the calculation of the wind effect on the structures. A high pressure coefficient value leads to an increase of the construction weight and subsequently to an increase in the construction cost. The EC1 in conjunction with EN 13031-1:2001, which is specialized for greenhouses, gives values for this coefficient. This value must satisfy two requirements: the safety of the structure and a reduced construction cost. In this paper, the Navier - Stokes and continuity equations are solved numerically with the finite element method (Galerkin Method) in order to simulate the two dimensional, incompressible, viscous air flow over the vaulted roofs of single span and twin-span with eaves livestock greenhouses' structures, with a height of 4.5 meters and with length of span of 9.6 and 14 m. The simulation was carried out in a wind tunnel. The numerical results of pressure coefficients, as well as, the distribution of them are presented and compared with data from Eurocodes for wind actions (EC1, EN 13031-1:2001). The results of the numerical experiment were close to the values given by the Eurocodes mainly on the leeward area of the roof while on the windward area a further segmentation is suggested.

• 한국공간구조학회:학술대회논문집
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• 한국공간구조학회 2008년도 춘계 학술발표회 논문집
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• pp.15-18
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• 2008

대공간 구조는 3차원적인 힘의 흐름과 면내력에 의해 외부하중에 대한 저항능력을 확보하는 형태 저항형 구조로서, 구조물 자체의 곡률을 이용하여 면외방향으로 작용하는 외력을 주로 면내력으로 저항할 수 있게한 구조시스템이다. 그러므로, 연성구조물의 일종인 막구조물은 대공간 구조물을 보다 효과적으로 구축할 수 있다. 이러한 막구조물은 지진이나 고정하중에 의한 영향보다 바람의 의한 영향이 매우 중요하다고 볼 수 있다. 또한, 풍하중은 주변 환경 및 구조물의 형태에 따라 그 크기가 매우 다르게 나타난다. 본 논문에서는, 우리나라에서 풍하중의 영향을 가장 많이 받은 지역들 중에 건설된, 2개 경기장의 설계 풍하중과 풍동실험 결과값들을 비교 검토해 보고자 한다.

• 대한기계학회논문집
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• 제18권6호
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• pp.1582-1589
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• 1994

The characteristics Prandt1-Meyer expansion of supersonic flow with condensation through a wavy wall in a channel are investigated by experiment and numerical direct marching method of characteristics. In the present study, for the case of moist air flow in the type of indraft supersonic wind tunnel, the dependency of location of formation and reflection of the oblique shock wave generated by the wavy wall and the distribution of flow properties, on the specific humidity and temperature at the entrance of wavy wall and the attack angle of the wavy wall to the main stream is clarified by schlieren photograph, distribution of static pressure and Mach number, and plots of numerical results. Also, we confirm that the wavy wall plays an important key role in the formation of oblique shock wave, and that the effect of condensation on the flow field appears apparently.

• 터널과지하공간
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• 제21권6호
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• pp.518-525
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• 2011

본 연구에서는 고준위 방사성 폐기물 처분장의 특징인 높은 고도 차이와 폐기물에서 발생하는 발열량에 따른 자연 환기력을 계산하고 이를 바탕으로 자연 환기량을 계산하였다. 고준위 방사성 폐기물 처분장은 열엔진과 유사한 폐쇄 싸이클의 열역학적인 과정을 따른다고 볼 수 있다. 지하처분장내 고준위 폐기물의 발열에 의한 열이 공기에 추가되고 이로 인해 공기가 upcast 수직갱을 통해 위로 올라가는 동안 팽창됨에 따라 주위에 일을 하고, 이때 한 일에 의해 첨가된 열의 일부분은 임시로 기계적 에너지로 변함으로서 공기의 흐름을 촉진할 수 있다. 이는 처분장 내에서 지속적이고 강력한 열원이 존재한다면 자연 지속적인 공기의 싸이클적 흐름을 가능하게 할 것이다. 이를 바탕으로 고준위 방사성 폐기물의 심지층 처분시 발생되는 자연 환기량을 수학적 방법으로 계산한 결과 굴뚝효과에 의하여 폐기물 발열량에 따라 $74{\sim}183$Pa의 자연 환기력이 계산되고 이에 따른 자연 환기량은 $92.5{\sim}147.7m^3/s$이 계산되었다. 또한 CFD의 자연환기량 해석결과는 $82{\sim}143m^3/s$로서 수학적인 방 법과 비교하여 매우 비슷한 결과를 나타내었다.

• Wind and Structures
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• 제18권5호
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• pp.567-598
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• 2014

In this paper, wind induced aerodynamic loads on a standard tall building have been evaluated through large-eddy simulation (LES) technique. The flow parameters of an open terrain were recorded from the downstream of an empty boundary layer wind tunnel (BLWT) and used to prescribe the transient inlet boundary of the LES simulations. Three different numerically generated inflow boundary conditions have been investigated to assess their suitability for LES. A high frequency pressure integration (HFPI) approach has been employed to obtain the wind load. A total of 280 pressure monitoring points have been systematically distributed on the surfaces of the LES model building. Similar BLWT experiments were also done to validate the numerical results. In addition, the effects of adjacent buildings were studied. Among the three wind field generation methods (synthetic, Simirnov's, and Lund's recycling method), LES with perturbation from the synthetic random flow approach showed better agreement with the BLWT data. In general, LES predicted peak wind loads comparable with the BLWT data, with a maximum difference of 15% and an average difference of 5%, for an isolated building case and however higher estimation errors were observed for cases where adjacent buildings were placed in the vicinity of the study building.

• 한국소음진동공학회논문집
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• 제13권2호
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• pp.83-91
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• 2003

Pantograph design Process must be considered in terms of stability of aerodynamics and reduction of aeroacoustics. Furthermore pantograph needs to be insensible to severe circumstance condition like typhoon, tunnel, a change of season. In this paper, robust design of panhead sections is conducted based on the Taguchi's design of experiment method. In the aeroacoustic noise analysis, an acoustic analogy using the Ffowcs Williams and Hawkings(FW-H) equation is used to calculate the flow induced sound pressure level in aeroacoustics. From the near-field CFD analysis data, the far-field noise is predicted at the positions of 25 m away from Pantograph. Based on aerodynamic(CFD) and aeroacoustic(FW-H) analysis data, the optimal sizing and Positioning of panhead elements are determined using robust design optimization method. Design parameters such as thickness, length and radius are controllable factors, while outdoor air temperature and atmospheric pressure are considered as uncontrollable factors in the context of Taguchi's approach. A number of CFD simulation and aeroacoustic analysis are performed based on orthogonal arrays. In this paper, two-step optimization method is used as a parameter design procedure. It is executed using signal to noise(S/N) ratio and analysis of means(ANOM) method. So Thus, an optimal level of design parameters Is extracted to minimize the disconnection ration between contact strips and catenary system, and reduce the far-field aeroacoustic noise.