• 제목/요약/키워드: scaled model tunnel

검색결과 135건 처리시간 0.02초

축소형 풍력터빈 풍동시험-축소효과 보상기법 (Wind Tunnel Test for Scaled Wind Turbine Model (Scale effect correction))

  • 조태환;김양원;박영민;장병희
    • 신재생에너지
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    • 제4권2호
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    • pp.87-93
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    • 2008
  • Wind tunnel test for the 12% scaled model of NREL Phase VI wind turbine was conducted in KARI low speed wind tunnel for $2006{\sim}2007$. The 1st and 2nd test was designed to find out the wind tunnel test method for the blade manufacturing accuracy and surface treatment method by using the composite and aluminum blades. And the 3rd test was designed to study the scale effect. The chord extension method which was used for Bo-105 40% scaled model was adapted for scale effect correction. Test results shows that the chord extension method works well for the torque slope but the maximum torque for scaled model is about 8% below than the real scale model. New correction method to correct this offset was proposed.

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축소모형실험을 통한 근접터널의 거동에 관한 연구 (A Study on the Behavior of a Closely-Spaced Tunnel by Using Scaled Model Tests)

  • 안현호;최정인;이석원;심성현
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2008년도 춘계 학술발표회 초청강연 및 논문집
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    • pp.189-198
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    • 2008
  • Lots of roadway tunnel have been almost constructed in forms of closely-spaced tunnel in korea. If closely-spaced tunnel is not constructed at a sufficient distance between tunnels, the problem of stability can occur. However, the case that can not secure a sufficient distance between tunnels can occur due to a difficulty in buying a lot and an issue of popular complaint and environmental disruption. Generally, tunnels are not influenced by each other when a center distance between tunnels is two times longer than tunnel diameter under the complete elastic ground and five times under the soft ground. In this study, the scaled model tests of closely-spaced tunnel by using homogeneous material were performed and induced displacements were measured around the tunnel openings during excavation. The influence of distance between tunnels on the behavior of closely-spaced tunnel was investigated.

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삼병렬 터널의 안정성 검토를 위한 모형실험 연구 (A Study for the Stability Investigation of Three Parallel Tunnels Using Scaled Model Tests)

  • 김종우;배우석
    • 터널과지하공간
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    • 제18권4호
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    • pp.300-311
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    • 2008
  • 삼병렬 터널은 3개의 터널이 서로 나란히 배열되는 형태의 터널이다. 본 연구에서는 터널간 이격거리, 터널단면 형상, 지보조건, 지반조건 등이 서로 다른 7가지 삼병렬 터널 모형들에 대한 축소모형실험을 통하여 모형별 균열개시압력과 터널 주변지반의 변형거동을 조사하였다. 터널간 이격거리가 작은 모형일수록 낮은 압력 수준에서 필러의 파괴가 일어나고 터널의 내공변형량도 증가하여 터널의 안정성은 감소하였다. 터널단면의 형상이 아치형, 편평아치형, 사각형인 모형들 중에서 사각형 단면을 가진 터널의 안정성이 가장 작았으며, 천반곡률반경이 작은 아치형 터널이 편평아치형 터널보다 안정성이 우수하였다. 터널의 천장부에 모형 록볼트를 설치한 모형은 무지보 터널 모형에 비하여 균열개시압력이 클 뿐만 아니라 천단침하량도 적게 나타나 지보의 효과를 확인할 수 있었다. 이방성 암반내 터널 모형은 등방성 모형과 매우 다른 변형거동을 나타내었으며, FLAC을 사용한 수치해석 결과는 모형실험의 결과와 정성적으로 부합하였다.

터널 단면크기에 따른 콘크리트 라이닝 타설 방법에 대한 실험적 연구 (Model test on concrete placement method of tunnel lining due to tunnel size)

  • 김상환;신범석;박인준
    • 한국터널지하공간학회 논문집
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    • 제11권3호
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    • pp.213-221
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    • 2009
  • 본 논문은 콘크리트 라이닝의 배면공동 현상, 초기 균열 등과 같은 콘크리트 라이닝 타설시 문제점들을 해결하기 위해 개선 방안을 제시하고 이를 단면크기의 변화에 따른 영향을 연구하였다. 연구를 수행하기 위해 초기 균열 형태와 발생 원인에 대한 분석을 실시하였으며 균열발생 최소화를 위한 개선된 타설 방안을 제시하였다. 제시한 타설 방안의 효율성 및 터널 단면크기에 따른 영향을 확인하기 위하여 기존의 1/20 축소모형실험 및 1/7 축소모형실험을 실시하여 타설율을 비교 분석하였다. 이에 따른 실험 결과는 기존의 타설 방안의 경우 1/20 축소모형실험 보다 1/7 축소모형실험의 타설율이 증가하여 차이를 보였지만 개선된 타설 방안의 경우 유사한 타설율을 나타내 2가지 실험 모두 신뢰성을 갖는 것으로 판단된다.

입자 유동 해석(PFC)을 통한 근접터널의 거동에 관한 연구 (A Study on the Behavior of a Closely-spaced Tunnel by Using Particle Flow Code)

  • 서병욱;조선아;정선아;이석원
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2008년도 춘계 학술발표회 초청강연 및 논문집
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    • pp.159-169
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    • 2008
  • In general, it is considered that a pillar between closely-spaced tunnel is sensitive for stress concentration. Stability of a pillar is key factor for excavation of closely-spaced tunnel. In this paper, the study is focused on tracing the behaviors, displacement and plotting damages around tunnels that is modelled with Particle Flow Code, $PFC^{2D}$. Parametric study was performed with changing distance between center of tunnels and coefficient of earth pressure(K). Scaled-model tests were also carried out to validate a numerical analysis model. It was found that $PFC^{2D}$ could show dynamic visualized result in quite good agreement with the experimental test.

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Evaluation of failure mode of tunnel-type anchorage for a suspension bridge via scaled model tests and image processing

  • Seo, Seunghwan;Lim, Hyungsung;Chung, Moonkyung
    • Geomechanics and Engineering
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    • 제24권5호
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    • pp.457-470
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    • 2021
  • In this study, the pull-out behavior of a tunnel-type anchorage for suspension bridges was investigated using experimental tests and image processing analyses. The study focused on evaluating the initial failure behavior and failure mode of the tunnel-type anchorage. In order to evaluate the failure mode of tunnel-type anchorage, a series of scaled model tests were conducted based on the prototype anchorage of the Ulsan Grand Bridge. In the model tests, the anchorage body and surrounding rocks were fabricated using a gypsum mixture. The pull-out behavior was investigated under plane strain conditions. The results of the model tests demonstrate that the tunnel-type anchorage underwent a wedge-shaped failure. In addition, the failure mode changed according to the differences in the physical properties of the surrounding rock and the anchorage body and the size of the anchor plate. The size of the anchor plate was found to be an important parameter that determines the failure mode. However, the difference in physical properties between the surrounding rock and the anchorage body did not affect its size. In addition, this study analyzed the initial failure behavior of the tunnel-type anchorage through image analysis and confirmed that the failure was sequentially transferred from the inside of the tunnel to the surrounding rock according to the image analysis. The reasonable failure mode for the design of the tunnel-type anchorage should be wedge-type rather than pull-out type.

NREL 풍력터빈 블레이드 20% 축소모델 풍동시험 결과 (Wind tunnel test for the 20% scaled down NREL wind turbine blade)

  • 조태환;김철완;김양원;노주현
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2011년도 추계학술대회 초록집
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    • pp.33.2-33.2
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    • 2011
  • The 'NREL Phase VI' model with a 10.06m diameter was tested in the NASA Ames tunnel to make a reference data of the computational models. The test was conducted at the one rotational speed, blade tip speed 38m/s and the Reynolds number of the sectional airfoils in that test was around 1E6. The 1/5 scale down model of the 'NREL Phase VI' model was used in this paper to study the power characteristics in low Reynolds number region, 0.1E6 ~ 0.4E6 which is achievable range for the conventional wind tunnel facilities. The torque generated by the blade was directly measured by using the torque sensor installed in the rotating axis for a given wind speed and rotational speed. The power characteristics below the stall condition, lambda > 4, was presented in this paper. The power coefficient is very low in the condition below the Re. 0.2E6 and rapidly increases as the Re. increases. And it still increases but the variation is not so big in the condition above the Re. 0.3E6. This results shows that to study the performance of the wind turbine blade by using the scaled down model, the Re. should be larger than the 0.3E6.

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Use of large-scale shake table tests to assess the seismic response of a tunnel embedded in compacted sand

  • Zhou, Hao;Qin, Xiaoyang;Wang, Xinghua;Liang, Yan
    • Earthquakes and Structures
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    • 제15권6호
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    • pp.655-665
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    • 2018
  • Shield tunnels are widely used throughout the world. However, their seismic performance has not been well studied. This paper focuses on the seismic response of a large scale model tunnel in compacted sand. A 9.3 m long, 3.7 m wide and 2.5 m high rigid box was filled with sand so as to simulate the sandy soil surrounding the tunnel. The setup was excited on a large-scale shake table. The model tunnel used was a 1:8 scaled model with a cross-sectional diameter of 900 mm. The effective shock absorbing layer (SAL) on the seismic response of the model tunnel was also investigated. The thickness of the tunnel lining is 60 mm. The earthquake motion recorded from the Kobe earthquake waves was used. The ground motions were scaled to have the same peak accelerations. A total of three peak accelerations were considered (i.e., 0.1 g, 0.2 g and 0.4 g). During the tests, the strain, acceleration and soil pressure on the surface of the tunnel were measured. In order to investigate the effect of shock absorbing layer on the dynamic response of the sand- tunnel system, two tunnel models were set up, one with and one without the shock absorbing layer of foam board were used. The results shows the longitudinal direction acceleration of the model tunnel with a shock absorbing layer were lower than those of model tunnel without the shock absorbing layer, Which indicates that the shock absorbing layer has a beneficial effect on the acceleration reduction. In addition, the shock absorbing layer has influence on the hoop strain and earth pressure of the model tunnel, this the effect of shock absorbing layer to the model tunnel will be discussed in the paper.

소형 저속 풍동에서 NASA 표준 연구 모형의 모형지지부 효과 연구 (Study on Model Support Interference of the Scaled NASA Common Research Model in Small Low Speed Wind Tunnel)

  • 김남균;조철영;고성호
    • 한국추진공학회지
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    • 제24권5호
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    • pp.56-64
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    • 2020
  • 29.7% 축소 NASA 표준 연구 모형에 대하여 소형 저속 풍동에서 시험을 수행하였다. 풍동시험 모형은 NASA Langley 연구소와 AIAA 항력추정 워크숍 위원회의 지침에 따라 알루미늄으로 제작하였다. 풍동의 능력 한계 등으로 상대적으로 낮은 레이놀즈수인 0.3 × 106 에서 정적 힘과 모멘트를 측정하였다. 세 가지 타입(핀 스팅, 블레이드 스팅, 벨리 스팅) 모형지지부에 대하여 피칭모멘트를 비교하였다. 보정된 벨리 스팅과 핀 스팅에 의한 피칭모멘트 보정량은 비슷하였으며 블레이드 스팅에 의한 피칭모멘트 값이 가장 적었다.

쌍굴터널 주변지반의 변형거동에 관한 모형실험 연구 (A Study on the Deformation Behaviors around Twin Tunnels Using Scaled Model Tests)

  • 김종우;박지용
    • 터널과지하공간
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    • 제14권5호
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    • pp.381-390
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    • 2004
  • 본 연구에서는 터널간 이격거리, 지반종류, 하중조건 등이 서로 다른 11가지 쌍굴터널 모형에 대한 축소모형실험을 통하여 터널 주변지반의 변형거동을 조사하였다. 이를 위해 모래, 석고, 물의 중량비를 달리한 모형재료에 대한 물성 실험을 통해 모형재료의 특성을 연구하였다. 쌍굴터널 사이의 이격거리가 좁은 모형일수록 낮은 압력 수준에서 균열이 개시되었고 필러의 spatting현상도 잘 발달하였으며 터널의 내공변형량도 증가하였다. 경암모형은 연암 모형에 비해 평균 50% 이상 큰 하중에서 균열이 개시되었고 동일 하중하에서 내공변형량도 2배정도 작게 나타났다. 모형터널의 파괴 및 변형양상은 측압 하중조건에 따라 매우 상이하게 나타났으며, FLAC을 사용한 수치해석 결과는 모형실험의 결과와 정성적으로 부합하였다.