• Title/Summary/Keyword: Wind Tunnel Experiment

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An Experimental Analysis of the Structural Stability Analysis of a Container Crane according to the change of the Boom Shape (붐 형상 변화에 따른 컨테이너 크레인 구조 안정성의 실험적 해석)

  • Lee S.W.;Han D.S.;Shim J.J.;Han G.J.;Kim T.H.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2006.05a
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    • pp.371-372
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    • 2006
  • This study was carried out to analyze the effect of wind load on the structural stability of a container crane according to the change of the boom shape using wind tunnel test and provide a container crane designer with data which can be used in a wind resistance design of a container crane assuming that a wind load 75m/s wind velocity is applied in a container crane. Data acquisition conditions for this experiment were established in accordance with the similarity. The scale of a container crane dimension, wind velocity and time were chosen as 1/200, 1/13.3 and 1/15. And this experiment was implemented in an Eiffel type atmospheric boundary layer wind tunnel with $11.52m^2$ cross-section area. Each directional drag and overturning moment coefficients of a container crane according to the change of the boom shape were investigated.

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Estimation of Topographic Effects over 3-Dimensional Hills through Wind Tunnel Tests (풍동실험을 이용한 3차원 산악지형의 풍속할증평가)

  • Cho, Kang-Pyo;Jeong, Seung-Hwan;Cho, Gi-Sung
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2007.04a
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    • pp.745-750
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    • 2007
  • This paper presents investigation of topographic effects over isolated 3-dimensional hills through wind tunnel experiments in a boundary layer wind tunnel. Topographic models having five different slopes of $5.71^{\circ},\;11.31^{\circ},\;16.70^{\circ},\;21.80^{\circ}$, and $26.57^{\circ}$, which were based on KBC(2005), were taken into account in the study. The maximum topographic factor and the range of topographic effect from the experiment were compared with those from worldwide major codes and standards, such as ASCE-7-02, AS/NZS-1170.2:2002, ISO4354(1997), and KBC(2005). From the comparison of major codes and standards, in the vertical region of topographic effect, the gentler the slope was. the more different the topographic factors and ranges of topographic effect were, but the steeper the slope was, the more similar they were. It was found from the experimental study that the region of topographic effect in the slope in the across wind direction was greater than the regions of major codes and standard. Also, the gentler the slope was. the larger the topographic factor from the experiment was than the factors of major codes and standards.

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Direct identification of aeroelastic force coefficients using forced vibration method

  • Herry, Irpanni;Hiroshi, Katsuchi;Hitoshi, Yamada
    • Wind and Structures
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    • v.35 no.5
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    • pp.323-336
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    • 2022
  • This study investigates the applicability of the direct identification of flutter derivatives in the time domain using Rational Function Approximation (RFA), where the extraction procedure requires either a combination of at least two wind speeds or one wind speed. In the frequency domain, flutter derivatives are identified at every wind speed. The ease of identifying flutter derivatives in the time domain creates a paradox because flutter derivative patterns sometimes change in higher-order polynomials. The first step involves a numerical study of RFA extractions for different deck shapes from existing bridges to verify the accurate wind speed combination for the extraction. The second step involves validating numerical simulation results through a wind tunnel experiment using the forced vibration method in one degree of freedom. The findings of the RFA extraction are compared to those obtained using the analytical solution. The numerical study and the wind tunnel experiment results are in good agreement. The results show that the evolution pattern of flutter derivatives determines the accuracy of the direct identification of RFA.

A 6 m cube in an atmospheric boundary layer flow -Part 1. Full-scale and wind-tunnel results

  • Hoxey, R.P.;Richards, P.J.;Short, J.L.
    • Wind and Structures
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    • v.5 no.2_3_4
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    • pp.165-176
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    • 2002
  • Results of measurements of surface pressure and of velocity field made on a full-scale 6 m cube in natural wind are reported. Comparisons are made with results from boundary-layer wind-tunnel studies reported in the literature. Two flow angles are reported; flow normal to a face of the cube (the $0^{\circ}$ case) and flow at $45^{\circ}$. In most comparisons, the spread of wind-tunnel results of pressure measurements spans the full-scale measurements. The exception to this is for the $0^{\circ}$ case where the roof and side-wall pressures at full-scale are more negative, and as a result of this the leeward wall pressures are also lower. The cause of this difference is postulated to be a Reynolds Number scale effect that affects flow reattachment. Measurements of velocity in the vicinity of the cube have been used to define the mean reattachment point on the roof centre line for the $0^{\circ}$ case, and the ground level reattachment point behind the cube for both $0^{\circ}$ and $45^{\circ}$ flow. Comparisons are reported with another full-scale experiment and also with wind-tunnel experiments that indicate a possible dependency on turbulence levels in the approach flow.

A Study on Wind Tunnel Experiment Education using 3D Printing (3D 프린팅을 활용한 풍동실험 교육 연구)

  • Lee, Yebin;Choi, Younseok
    • Journal of Engineering Education Research
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    • v.27 no.5
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    • pp.3-9
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    • 2024
  • This paper analyzed the effectiveness of wind tunnel test with 3D printing technology. Existing tests were limited to testing theoretical results with simplified models. In order to apply a more efficient production method and utilize it in various experiments, research on diverse applications was conducted in small and medium-sized wind tunnels. As a result, it was analyzed that 3D printing models can be effectively applied to wind tunnel tests, and it is expected that advanced aerospace engineering education will be possible through this approach.

A Study on the Development and Performance Test of Supersonic Wind Tunnel for Education (교육용 초음속 풍동 개발 및 성능검증에 관한 연구)

  • Lee, Jin-Ho;Huh, Choul-Jun;Bae, Ki-Joon;Bae, Yung-Woo;Byun, Yung-Hwan;Lee, Jae-Woo;Chang, Jo-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.8
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    • pp.129-137
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    • 2004
  • A small size - low priced supersonic wind tunnel of which test section size is 30mm by 35.6mm and run time is 20sec is developed. This educational supersonic wind tunnel is an intermittent blowdown type with an exchangeable nozzle block. In this study, the proper sized and low priced commercial parts are used to reduce the total cost of supersonic wind tunnel. A nozzle design and small supersonic wind tunnel design process has been established, and it is confirmed that a given supersonic flow field has been obtained and proved by experiment.

A Study on the Estimation of the Structural Stability of a Container Crane according to the Change of the Boom Shape using Wind Tunnel Test (풍동실험을 이용한 붐 형상 변화에 따른 컨테이너 크레인 구조 안정성 평가에 관한 연구)

  • Lee Seong-Wook;Han Geun-Jo;Han Dong-Seop;Kim Tae-Ryung
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2006.06b
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    • pp.311-316
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    • 2006
  • This study was carried out to analyze the effect of wind load on the structural stability of a container crane according to the change of the boom shape using wind tunnel test and provided a container crane designer with data which can be used in a wind resistance design of a container crane assuming that a wind load at 75m/s wind velocity is applied on a container crane. Data acquisition conditions for this experiment were established in accordance with the similarity. The scale of a container crane dimension, wind velocity and time were chosen as 1/200, 1/13.3 and 1/15. And this experiment was implemented in an Eiffel type atmospheric boundary-layer wind tunnel with $11.25m^2$ cross-section area. Each directional drag and overturning moment coefficients were investigated and uplift forces at each supporting point due to the wind load were analyzed.

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Wind tunnel experiments of a building model incorporating viscous-damping walls

  • Pan, Austin D.E.;Yeung, Ngai
    • Wind and Structures
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    • v.4 no.3
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    • pp.261-276
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    • 2001
  • This paper presents an experimental study on the effectiveness of viscous-damping walls in controlling the wind-induced vibrations of a building model. A simple four-story building model, square in plan, was constructed for wind tunnel study. In this paper the description of the model, its instrumentation, and the experimental set-up and methodology are reported. The effectiveness of viscous-damping walls in reducing vibrations was investigated for different fluid levels in the walls, and at varying wind speeds and attack angles. The results show that viscous-damping walls are highly effective in most cases.

An Experimental Study on the Responsiveness of Sprinkler Heads (스프링클러헤드 응답성에 관한 실험적 연구)

  • 김동석;박용일;박희용
    • Fire Science and Engineering
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    • v.7 no.2
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    • pp.3-12
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    • 1993
  • The closed type sprinkler head is a component of sprinkler system for fire protection. The purpose of this study is to inverstigate the influence factors of the responsiveness of the head by heated wind tunnel experiment. As the result of this study, it was found that response time index and conduction parameter showed the same characteristic quantitative changes to head types and test methods.

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Wind Force Coefficients Computation of Gantry Crane by Wind Tunnel Experiment and Structural Analysis of the Crane (풍동실험에 의한 갠트리 크레인의 풍력계수 산출과 구조 해석)

  • Lee, Jae-Hwan;Kim, Tae-Wan;Jang, In-Geun;Han, Soon-Hung
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.2
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    • pp.165-170
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    • 2011
  • In this paper, wind force coefficient by wind tunnel experiment is obtained to compute the accurate wind force of the gantry crane model to be used for mobile harbor ship. The first crane model was tested under 20, 30, 40, 52m/s, partially 58m/s and the wind force coefficient is about 2.0 which is very close to the suggested theoretical value. The other is the more reliable crane model and tested under 20, 30, 40m/s also giving the similar realistic wind force coefficient. Also structural analysis of crane model was performed giving the reliable stress level. Since the rolling effect is important for mobile harbor ship, the safety of the crane on the ship needs to be guaranteed. For this, using the computed reaction forces, a tie-down design is suggested which connects the crane and ship to resist the turnover motion of the crane.