• 제목/요약/키워드: Scaled model test

검색결과 365건 처리시간 0.029초

축소모형실험 폭원으로서 도폭선의 폭력조절 (Detonating Cord as a Controllable Source for Scaled Model Blasting Test)

  • 양형식;김종관;최미진;최병희;류창하
    • 터널과지하공간
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    • 제17권4호
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    • pp.295-300
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    • 2007
  • 도폭선의 길이를 조절하여 폭력이 조절되도록 축소모형 실험하는 방법을 제안하였으며 콘크리트 블록의 발파에 적용하여 타당성을 검토하였다. 제안된 방법은 폭원 조절이 가능하고 또 축소모형실험 방법으로서 타당한 것으로 판단된다. 또 폭발열을 이용하여 산정한 폭원 축소율은 상당한 근거가 있는 것으로 판단되었다.

폭원의 축소율 산정과 축소모형 실험에의 적용 (Scale Factor of Explosives and Application on Scaled Model Test of Demolition Blasting)

  • 정도영;양형식
    • 화약ㆍ발파
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    • 제22권4호
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    • pp.1-6
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    • 2004
  • 본 연구에서는 발파해체에 대한 축소모형실험의 폭원에 대한 차원과 축소율을 산정하고, 이로부터 축소모형실험의 적정 길이의 축소율을 고찰하였다. 그 결과 길이 축소비를 1/4로 할 때 축원의 축소율은 1/256로 모형실험과 실제 구조물에서 사용한 화약량의 비로 구한 축소율과 유사한 값을 보였다. 길이 축소율은 1/4 이상으로 하는 것이 바람직하다고 판단된다

축소형 틸트로터 무인기의 안전줄 호버 시험 (Tethered Hover Test for Small Scaled Tilt-rotor UAV)

  • 박범진;유창선;장성호;최성욱;구삼옥;강영신
    • 한국항공운항학회지
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    • 제15권4호
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    • pp.9-16
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    • 2007
  • Tilt rotor aircraft can take off and land vertically and cruise faster than any other helicopter. A scaled flight demonstration model of a tilt rotor aircraft has been developed by KARI. Because the flight characteristics of tilt rotor are not well known, the developed scaled model would be helpful to evaluate flight control algorithm of a full scale aircraft. The tethered hover test has been performed in order to improve hover flight characteristics of tilt rotor aircraft prior to flight test of the small scaled model. During the tethered hover test, the performance of rotor speed governor, rate SAS (Stability Augmentation System) and control surface mixers have been evaluated. We expect that the results of real flight hover test would be quite same as tethered hover test. Therefore the tethered hover test results will reduce the risk of flight test properly by fixing some of hidden problems which might occur during the flight test. This paper presents the results of tethered hover test in detail and shows how it could be final ground test before flight test. The control mixer gain and rate SAS feedback gains were modified in order to get higher controllability and stability during the tethered hover flight. The rotor governor showed that it could keep rotor RPM constant with very small deviation even during severe pilot collective input change. The tethered hover test results gave pilot and engineers confirmation and experience about the scheduled flight test.

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Evaluation on bridge dynamic properties and VIV performance based on wind tunnel test and field measurement

  • Yang, Yongxin;Ma, Tingting;Ge, Yaojun
    • Wind and Structures
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    • 제20권6호
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    • pp.719-737
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    • 2015
  • Full scale measurement on the structural dynamic characteristics and Vortex-induced Vibrations (VIV) of a long-span suspension bridge with a central span of 1650 m were conducted. Different Finite Element (FE) modeling principles for the separated twin-box girder were compared and evaluated with the field vibration test results, and the double-spine model was determined to be the best simulation model, but certain modification still needs to be made which will affect the basic modeling parameters and the dynamic response prediction values of corresponding wind tunnel tests. Based on the FE modal analysis results, small-scaled and large-scaled sectional model tests were both carried out to investigate the VIV responses, and probable Reynolds Number effects or scale effect on VIV responses were presented. Based on the observed VIV modes in the field measurement, the VIV results obtained from sectional model tests were converted into those of the three-dimensional (3D) full-scale bridge and subsequently compared with field measurement results. It is indicated that the large-scaled sectional model test can probably provide a reasonable and effective prediction on VIV response.

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.

CANDU-6 감속재 탱크 모형의 유동장 전산해석 및 예비측정 (Computational Flow Analysis and Preliminary Measurement for the CANDU-6 Moderator Tank Model)

  • 차재은;최화림;이보욱;김형태
    • 한국가시화정보학회지
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    • 제10권3호
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    • pp.30-36
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    • 2012
  • We are planning to construct a scaled-down moderator facility to simulate the CANDU-6 moderator circulation phenomena during steady state operating and accident conditions. In the present work a preliminary experiment using a 1/40 scaled-down moderator tank has been performed to investigate the anticipated problems of the flow visualization and measurement in the planning scaled-down moderator facility. We shortly describe CFD analysis result for the 1/40 scaled-down test model and the flow measurement techniques used for this test facility under isothermal flow conditions. The Particle Image Velocimetry (PIV) method is used to visualize and measure the velocity field of water in a transparent Plexiglas tank. Planar Laser Induced Fluorescence (PLIF) technique is used to evaluate the feasibility of temperature field measurement in the range of $20-40^{\circ}C$ of water temperature using an one-color method.

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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한국인 체형을 가진 보행자와 차량의 충돌 해석 (Analysis of Car-Pedestrian Collisions Using Scaled Korean Dummy Models)

  • 신동한;김광훈;손권
    • 한국정밀공학회지
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    • 제24권5호
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    • pp.110-117
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    • 2007
  • According to the pedestrian protection regulations of Europe and Japan, the head injury must not exceed a limitation in the defined test condition for the protection of pedestrians from a vehicle crash. However, it is difficult to evaluate the performance of protection because each regulation has different test conditions such as dummy, impact speed and so on. This circumstance needs the development of a model that describes the anthropometry of the crash victim with a sufficient accuracy. We constructed scaled pedestrian dummies using MADYSCALE. Simulations were performed for various crash speeds and pedestrian postures. The scaled Korean dummies and HybridIII dummies were used to compare the pedestrian dynamic behaviors and head injury criteria during the collision. The HIC values of scaled korean dummies were found to be higher than those of Hybrid III dummies. The impact for gait posture was less than that for standing.

OMA testing by SLDV for FEM Updating

  • Milla, Brian-Mac;Mehdi Batel;Eddy Dascott;Ben Verbeeck
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 추계학술대회논문집
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    • pp.840-840
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    • 2003
  • Operational Modal Analysis (OMA) is a technique for identification of modal parameters by measurement of only the system's response. On many lightweight structures, such as load-speaker cones and disk drive read/write heads, is impossible or impractical to measure the input forces. Another characteristic of lightweight structure is their sensitivity to mass loading from sensors. The Scanning Laser Doppler Vibrometry(SLDV) allows response measurements to be taken without mass loading. One disadvantage of OMA testing compared to tradition input output modal testing is the OMA mode shapes are un-scaled. This means that the mode shape obtained from an OMA test can not used for analytical structural modification studies. However, the un-scaled mode shapes from an OMA test can be used to update a Finite Element Model (FEM). The updated FEM can then be used to analytically predict the effect of structural modifications. This paper will present the results of an OMA test performed on a simple plate and motor in operating conditions. The un-scaled mode shapes from this test will be used to update a FEM model of the system. The updated FEM model will be then be used to predict the effect of attaching a mass to the plate. The shapes predicted by the FEM for the modified system will be compared to a second OMA test on the modified system

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시뮬레이션과 축소모형에 의한 UPFC의 성능해석 (Performance Analysis of UPFC by Simulation & Scaled Hardware Model Test)

  • 한병문;박지용;정진규
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1999년도 하계학술대회 논문집 F
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    • pp.2475-2477
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    • 1999
  • This paper describes a simulation model and scaled hardware model to analyze the dynamic performance of Unified Power Flow Controller, which adjust flexibly the active and reactive power flow through the ac transmission line. The design of control system was developed using vector control method. The results of simulation and scaled hardware test show that the developed control system works accurately. And both models are very effective to analyze the dynamic performance of the Unified Power Flow Controller.

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