• Journal of Mechanical Science and Technology
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• 제15권12호
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• pp.1816-1821
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• 2001

Two-dimensional blow-down type supersonic wind tunnel was designed and built to investigate the transient behavior of the startup of a supersonic flow from rest. The contour of the divergent part of the nozzle was determined by the MOC calculation. The converging part of the nozzle, upstream of fille throat was contoured to make the flow uniform at the throat. The flow characteristics of the steady supersonic condition were visualized using the high-speed schlieren photography. The Mach number was evaluated from the oblique shock wave angle on a sharp wedge with halt angle of 5 degree. The measured Mach number was 2.4 and was slightly less than the value predicted by the design calculation. The initial transient behavior of the nozzle was recorded by a high-speed digital video camera with schlieren technique. The measured transition time from standstill to a steady supersonic flow was estimated by analyzing the serial images. Typical transition time was approximately 0.1sec.

• 생물환경조절학회지
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• 제7권1호
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• pp.9-14
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• 1998

본 연구에서는 인공광하의 풍동내에서 기류속도와 생육실내의 위치가 플러그묘 개체군의 생장에 미치는 효과를 분석하였다 기류속도가 증가하면 모개체군내에서의 상대습도는 감소하나, 포차는 증가한다. 이에 따라 증산이 활발하게 이루어져 잎에서의 수분포텐셜이 저하되며 묘개체군 위에서 공기역학적 저항이 감소함에 따라 확산계수가 높게 나타난다. 그 결과로서 0.93m.s$^{-1}$의 기류속도에서 줄기 길이, 줄기직경에 대한 줄기 길이의 비, 초장, 엽수는 유의성이 인정될 만큼 작게 나타났다. 묘개체군의 순광합성속도는 기류속도의 증가와 함께 증가되면서 0.7~0.9 m.s$^{-1}$에서 높게 나타났다. 생육실내의 위치 즉 기류의 진행방향을 따라 줄기 직경과 지하부 건물 중은 감소하였으나, 줄기 직경에 대한 줄기 길이의 비와 엽면적은 증가하는 것으로 나타났다. 이밖에 플러그묘의 생체중 또는 건물 중에 대한 T/R비는 기류속도의 변화와 무관하게 각각 2.8~3.5, 3.2~3.9로서 비슷하게 나타났으나, 건물율은 지상부에서 8.1~9.4, 지하부에서 10.1~10.9로서 지하부에서 다소 높게 나타났다. 그러므로 기류속도의 크기와 기류의 진행방향에 따라 묘개체군 위에서의 확산계수가 다르게 나타나며 이로 인하여 모개체군의 생장 차이가 나타남을 알 수 있다. 따라서 식물모공장과 같이 인공광을 이용한 반폐쇄 식물생산 시스템에서 품질이 균일한 모를 생산하려면 묘개체군의 미기상에 기초한 적정 환경조건의 확립이 요구된다.

• 문화기술의 융합
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• 제9권2호
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• pp.575-580
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• 2023

본 논문에서는 농업용 방제 드론을 이용하여, 균일 방제를 통해 병해충에 농작물을 방지하고자 한다. 방제가 수행되는 비행 고도는 4 m 로 고정하고, 비행 속도 4-5 m/sec. 범위에서 실험을 수행하였다. 방제사의 조종 습관 및 방법, 바람의 영향과 같이 환경적 요인이 작용하여 정량화된 방제 작업이 어렵다. 실험은 10 m 농지에서 감수지를 한 열에 1.25 m 간격으로 7 장씩 5 열을 10 m 간격으로 배치하고, 제안된 항공 살포 시스템을 적용하여 살포 실험을 수행하였다. 분사 노즐 중심으로 좌우측 약 3.75 m 지점에서부터 분사된 입자가 감소하기 시작하였다. 입자의 개수에 따라 유효 살포 폭은 약 7.5 m 영역으로 관찰되었으며, 제안된 살포 시스템이 균일 방제에 효과가 있음을 실험적으로 검증하였다.

• 생물환경조절학회지
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• 제4권1호
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• pp.32-42
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• 1995

1. 시설형태별 온도분포는 Type 1의 경우 지붕의 환기구가 없기 때문에 중력환기는 거의 일어나지 않고, 풍력환기에만 의존하게 되므로 풍속이 약한 경우는 온도가 상승하였다. Type 2 및 Type 3는 지붕의 환기구를 통하여 중력환기가 일어나기 때문에 대체로 온도 분포도 균일한 편으로 나타났다. 2. 시설형태별 평면 광분포는 Type 1가 가장 높고 Type 2, Type 3순으로 나타났다. 즉 일사투과율에 의한 지면 일사 도달율과 직접적으로 관련되기 때문에 Type 1, Type 2, Type 3순으로 지면온도 상승에 영향을 주었다. 3. 환기모델과 열수지 모델을 도입하여 환기량 및 실내온도 변화를 구한 결과, 시설형태별 풍속의 변화에 따른 내외기온차 변화는 Type 1이 가장 크고 Type 2, Type 3순이었다. Type 1의 경우 다른 형태에 비하여 풍속이 1 ㎧로 증가하면 급격히 내외기온차가 감소하였다. 4. 실측치를 사용하여 모델에 의한 풍속변화에 따른 환기량의 변화를 추정한 결과, Type 3 및 Type 2가 상대적으로 Type 1보다 낮은 경향을 나타냈다. 5. 전체적으로 개량형인 Type 2 및 Type 3은 관행형인 Type 1보다 효율적이라고 판단된다. 특히, 성력화의 차원에서 보면 Type 3이 Type 2보다 월등히 우수하기 때문에 자연적인 강우차단 능력이 보장된다면 Type 3이 Type 2보다 효율적이라고 사료된다.

• Wind and Structures
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• 제26권5호
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• pp.279-292
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• 2018

Inspired by the energy harvesting eel, a flexible flag behind a D-shape cylinder in a uniform viscous flow was simulated by using the immersed boundary method (IBM) along with low-speed wind tunnel experimentation. The flag in the wake of the cylinder was strongly influenced by the vortices shed from the upstream cylinder under the vortex-vortex and vortex-body interactions. Geometric and flow parameters were optimized for the flexible flag subjected to passive flapping. The influence of length and bending coefficient of the flexible flag, the diameters (D) of the cylinder and the streamwise spacing between the cylinder and the flag, on the energy generation was examined. Constructive and destructive vortex interaction modes, unidirectional and bidirectional bending and the different flapping frequency were found which explained the variations in the energy of the downstream flag. Voltage output and flapping behavior of the flag were also observed experimentally to find a more direct relationship between the bending of the flag and its power generation.

• Steel and Composite Structures
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• 제20권4호
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• pp.813-832
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• 2016

This research deals with the behavior of Composite Box Girder Bridges (CBGBs) subjected to environmental effects such as solar radiation, atmospheric temperature, and wind speed. It is based on temperature and thermal stress results, which were recorded hourly from a full-scale experimental CBGB segment and Finite Element (FE) thermal analysis. The Hemi-cube method was adopted to achieve the accuracy in temperature distributions and variations in a composition system during the daily environmental variations. Analytical findings were compared with the experimental measurements, and a good agreement was found. On the other hand, parametric investigations are carried out to investigate the effect of the cross-section geometry and orientation of the longitudinal axis of CBGB on the thermal response and stress distributions. Based upon individual parametric investigations, some remarks related to the thermal loading parameters were submitted. Additionally, some observations about the CBGB configurations were identified, which must be taken into account in the design process. Finally, this research indicates that the design temperature distribution with a uniform differential between the concrete slab and the steel girder is inappropriate for describing the thermal impacts in design objective.

• 한국항공운항학회지
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• 제11권1호
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• pp.41-55
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• 2003

A calibration jet system using separate blower is developed to calibrate a flow sensor effectively. Designed open circuit type mini calibration jet system, which has the dimension of $0.5m(W){\times}1.17m(H)$ is small compared with conventional calibration jet systems. The exit of nozzle has exchangeable contractions with a cross section area of $38.5cm^2$ , and a cross section area of $113.1cm^2$, respectively. The ranges of wind speed at exit of exchangeable nozzles are $7.5{\sim}42\;m/s$ and $1.8{\sim}16.5\;m/s$, respectively. The input power for the high pressure blower is 1.18kW. The turning vanes for corner was rolled flat plate parallel to the flow direction. The flow conditioning screen was located immediately downstream of the wide-angle diffuser. The honeycomb and two flow conditioning screens were located in the stagnation chamber. From the economical point of view and the simplicity of the calibration jet system set up and handling, it can be said that the developed calibration jet system is an effective calibration jet system. This system can also be used to calibrate the flow sensor with high resolution.

• 대한토목학회논문집
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• 제26권6A호
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• pp.1013-1022
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• 2006

본질적으로 두 개의 I형 거더를 가진 사장교는 공기역학적으로 불리한 특성을 가지고 있음에도 불구하고 경제적으로 유리하기 때문에 최근 우리나라에서 많이 건설되고 있다. 본 논문에서는 두 개의 I형 거더를 가지는 사장교의 실제 조건 하에서의 공기역학적 특성을 평가하기 위하여 영각, 난류강도, 감쇠비를 변화시켜가면서 단면모형실험을 수행하였다. 비틀림 강성이 다른 두 개의 상부 단면 형식이 시공단계 및 완공 후에 대하여 각각 조사되었고 교량의 공기역학적 특성을 향상시키기 위하여 3가지 형식의 페어링이 고려되었다. 연구결과, 전통적인 등류에서의 단면모형실험은 다소 비관적으로 공기역학적 거동을 평가하고 있으며 교량의 바람에 의한 응답은 난류강도와 구조감쇠비에 따라 현저하게 변화하는 것을 확인하였다. 본 연구에서 제시된 페어링은 와류진동 및 버페팅 진동을 감소시켰으며 또한, 플러터의 발생속도도 증가시켰다. 본 연구결과는 두 개의 I형 거더를 가지는 사장교의 내풍설계를 위한 많은 정보를 제공할 수 있을 것으로 기대된다.

• Wind and Structures
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• 제35권4호
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• pp.269-285
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• 2022

The pressure-mitigating effects of a high-speed train passing through a tunnel with a partially reduced cross-section are investigated via the numerical approach. A compressible, three-dimensional RNG k-ε turbulence model and a hybrid mesh strategy are adopted to reproduce that event, which is validated by the moving model test. Three step-like tunnel forms and two additional transitions at the tunnel junction are proposed and their aerodynamic performance is compared and scrutinized with a constant cross-sectional tunnel as the benchmark. The results show that the tunnel step is unrelated to the pressure mitigation effects since the case of a double-step tunnel has no advantage in comparison to a single-step tunnel, but the excavated volume is an essential matter. The pressure peaks are reduced at different levels along with the increase of the excavated earth volume and the peaks are either fitted with power or logarithmic function relationships. In addition, the Arc and Oblique-transitions have very limited gaps, and their pressure curves are identical to each other, whereas the Rec-transition leads to relatively lower pressure peaks in C_Pmax, C_Pmin, and ΔC_P, with 5.2%, 4.0%, and 4.1% relieved compared with Oblique-transition. This study could provide guidance for the design of the novel railway tunnel.

• 대한기계학회논문집B
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• 제22권6호
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• pp.860-873
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• 1998

In a low speed open-type wind tunnel, a group of parallel wakes downstream of two dimensional grid model consisting of several circular cylinders were experimentally investigated to study the response of the wake flows to the acoustic excitation, in hoping to promote the understanding of the underlying mechanism behind the gross flow change due to artificial excitation. In the unexcited wake flows, the development of the individual wakes behind cylinders was almost uniform for the ratio of the spacing to the cylinder diameter of s/d.geq.1.5. For smaller s/d, however, the jet streams issued through the gaps between the cylinders became biased in one side and the cylinders had wakes of different sizes. At s/d=1.25, the gap flow directions change in time, leading to unstable wake patterns. Further reduction in s/d made this unstable flip-flopping of the jets stable. The most effective excitation frequency was found to be in the Strouhal number range of St=0.5-0.6. This frequency was related to the vortex shedding. At s/d=1.75, the excitation frequency was 2 or 4 times the vortex shedding frequency. When the flow was excited at this frequency, the vortex sheddings were energized, and pairings between neighboring vortices were generated. Also, the merging process between individual wakes was accelerated. The unstable and unbalanced wake patterns at s/d=2.15 were made stable and balanced. The unstable and unbalanced wake patterns at s/d=2.15 were made stable and balanced. For smaller spacing of s/d .leq,1.0, the acoustic excitation became less effective in controlling the flow.