• 제목/요약/키워드: wind-tunnel measurement

검색결과 188건 처리시간 0.024초

저속풍동 시험부 속도교정에 관한 실험적 연구 (An Experimental Study of Test Section Velocity Calibration for Low-Speed Wind Tunnel)

  • 오세윤;이종건;김성철;김상호;안승기
    • 한국항공우주학회지
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    • 제40권3호
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    • pp.230-236
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    • 2012
  • 본 연구의 목적은 풍동 시험부의 속도산출에 필요한 속도측정시스템용 교정계수를 실험적으로 결정하는데 있었다. 교정실험은 국방과학연구소 저속풍동에서 표준 피토관을 이용하여 수행되었으며 이때의 교정속도 영역은 약 10~100 m/s이었다. 풍동교정실험결과의 유효성 평가를 위해 기존의 교정계수 측정결과와의 비교검토를 수행하였으며, 기존 교정 결과들과 잘 부합됨을 확인하였다.

Mechanism on suppression in vortex-induced vibration of bridge deck with long projecting slab with countermeasures

  • Zhou, Zhiyong;Yang, Ting;Ding, Quanshun;Ge, Yaojun
    • Wind and Structures
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    • 제20권5호
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    • pp.643-660
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    • 2015
  • The wind tunnel test of large-scale sectional model and computational fluid dynamics (CFD) are employed for the purpose of studying the aerodynamic appendices and mechanism on suppression for the vortex-induced vibration (VIV). This paper takes the HongKong-Zhuhai-Macao Bridge as an example to conduct the wind tunnel test of large-scale sectional model. The results of wind tunnel test show that it is the crash barrier that induces the vertical VIV. CFD numerical simulation results show that the distance between the curb and crash barrier is not long enough to accelerate the flow velocity between them, resulting in an approximate stagnation region forming behind those two, where the continuous vortex-shedding occurs, giving rise to the vertical VIV in the end. According to the above, 3 types of wind fairing (trapezoidal, airfoil and smaller airfoil) are proposed to accelerate the flow velocity between the crash barrier and curb in order to avoid the continuous vortex-shedding. Both of the CFD numerical simulation and the velocity field measurement show that the flow velocity of all the measuring points in case of the section with airfoil wind fairing, can be increased greatly compared to the results of original section, and the energy is reduced considerably at the natural frequency, indicating that the wind fairing do accelerate the flow velocity behind the crash barrier. Wind tunnel tests in case of the sections with three different countermeasures mentioned above are conducted and the results compared with the original section show that all the three different countermeasures can be used to control VIV to varying degrees.

HFFB technique and its validation studies

  • Xie, Jiming;Garber, Jason
    • Wind and Structures
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    • 제18권4호
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    • pp.375-389
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    • 2014
  • The high-frequency force-balance (HFFB) technique and its subsequent improvements are reviewed in this paper, including a discussion about nonlinear mode shape corrections, multi-force balance measurements, and using HFFB model to identify aeroelastic parameters. To apply the HFFB technique in engineering practice, various validation studies have been conducted. This paper presents the results from an analytical validation study for a simple building with nonlinear mode shapes, three experimental validation studies for more complicated buildings, and a field measurement comparison for a super-tall building in Hong Kong. The results of these validations confirm that the improved HFFB technique is generally adequate for engineering applications. Some technical limitations of HFFB are also discussed in this paper, especially for higher-order mode response that could be considerable for super tall buildings.

Wind tunnel study of wind structure at a mountainous bridge location

  • Yan, Lei;Guo, Zhen S.;Zhu, Le D.;Flay, Richard G.J.
    • Wind and Structures
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    • 제23권3호
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    • pp.191-209
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    • 2016
  • Wind tunnel tests of a 1/2200-scale mountainous terrain model have been carried out to investigate local wind characteristics at a bridge location in southeast Tibet, China. Flows at five key locations on the bridge at deck level were measured for 26 directions. It was observed that wind characteristics (including mean wind velocity and overall turbulence intensity) vary significantly depending on the approaching wind direction and measurement position. The wind inclination angle measured in the study fluctuated between $-18^{\circ}$ and $+16^{\circ}$ and the ratio of mean wind velocity to reference wind velocity was small when the wind inclination angles were large, especially for positive wind inclination angles. The design standard wind speed and the minimum critical wind speed for flutter rely on the wind inclination angle and should be determined from the results of such tests. The variation of wind speed with wind inclination angles should be of the asymmetry step type. The turbulence characteristics of the wind were found to be similar to real atmospheric flows.

풍동실험을 통한 배과원 방충망의 풍하중 및 항력계수 평가 (Evaluation of Wind Load and Drag Coefficient of Insect Net in a Pear Orchard using Wind Tunnel Test)

  • 송호성;유석철;김유용;임성윤
    • 한국농공학회논문집
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    • 제61권1호
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    • pp.75-83
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    • 2019
  • Fruit bagging is a traditional way to produce high-quality fruit and to prevent damage from insects and diseases. Growing pears by non-bagging is concerned about the damage from insect, it can be controlled by installing a insect net facility. Wind load should be considered to design the insect net facility because it has the risk of collapse due to the strong wind. So we carried out wind tunnel test for measurement of drag force, where the insect net with porosity about 65% is selected as an experimental subject. As a result of the test, drag force was measured to be 244.14 N when insect net area and wind speed are $1m^2$ and 22.7 m/s respectively. And, drag coefficients for the insect net were found to be about 0.55~0.57, which may be used as the preliminary data to design the insect net facilities at the orchard.

인공광하의 공정육묘용 풍동 설계 및 공정묘 개체군상의 공기역학적 특성 (Design of a Wind Tunnel for Plug Seedlings Production under Artificial Light and Aerodynamic Characteristics above Plug Stand)

  • 김용현;고재풍수
    • Journal of Biosystems Engineering
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    • 제21권4호
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    • pp.429-435
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    • 1996
  • A wind tunnel consisting of two air flow conditioners with polycarbonate pipes, a plant growth room, a suction fan and fan controller, and fluorescent lamps, was designed to investigate the interactions between the growth of plug seedlings under artificial light and their Physical environments. Light transmissivities in the plant growth room based on the photosynthetic photon flux density and photosynthetically active radiation was appeared to be 96.3% and 96.8%, respectively. Measurement showed a uniformity in the vertical profiles of air current speed at the middle and rear regions of plug trays in wind tunnel. This result indicated that the development of a wind tunnel based on the design criteria of the American Society of Mechanical Engineers was adequate. Air current speed inside the plug stand was significantly decreased due to the resistance by the leaves of plug seedlings and boundary layer developed over and below the plug stand. Driving force to facilitate the diffusion of gas inside the plug stand might be regarded as extremely low. Aerodynamic characteristics above the plug stand under artificial light were investigated. As the air current speed increased, zero plane displacement decreased but roughness length and frictional velocity increased. Zero plane displacement linearly increased with the average height of plug seedlings. The wind tunnel developed in this study would be useful to investigate the effects of air current speed on the microclimate over and inside the plug stand and to collect basic data for a large-scale plug production under artificial light in a semi-closed ecosystem.

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Wind tunnel study of plume dispersion with varying source emission configurations

  • Wittwer, Adrian R.;Loredo-Souza, Acir M.;Schettini, Edith B. Camano;Castro, Hugo G.
    • Wind and Structures
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    • 제27권6호
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    • pp.417-430
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    • 2018
  • The concentration fields in the proximities of a local gas emission source are experimentally analyzed in several combinations of wind incidences and source emissions. These conditions are determined by the plume buoyancy, emission velocity and incident flow wind speed. Concentration measurements are performed by an aspirating probe in a boundary layer wind tunnel. The analysis included the mean concentration values and the intensity of concentration fluctuations in a neutral atmospheric boundary layer flow. Different configurations are tested: an isolated stack in a homogeneous terrain and a stack with a bluff body in close proximity, located windward and leeward from the emission source. The experimental mean concentration values are contrasted with Gaussian profiles and the dilution factor is analyzed with respect to the empirical curves of the minimum dilution. Finally, a study on the plume intermittency is performed in a cross-sectional plane near the emission source. It is possible to highlight the following observations: a) plume vertical asymmetry in the case of an isolated emission source, b) significant differences in the dispersion process related to the relative location of the emission source and bluff body effects, and c) different probabilistic behavior of the concentration fluctuation data in a cross-sectional measurement plane inside the plume.

석회석 노천채광장의 분진 비산특성 (Dust Fall Property of Open Cut Limestone Mine)

  • 이상권;김복윤;조영도;김임호
    • 화약ㆍ발파
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    • 제17권2호
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    • pp.45-51
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    • 1999
  • 본 연구에서는 Dust Fall Sample을 설치하여 한라시멘트 옥계 채광현장의 천공, 발파작업시 발생되는 분진을 측정하고, 실험적인 방법으로 100m길이의 가설 풍동을 만들어 풍속별 비산거리 및 분진입도 분포 등을 파악하여 주변작업 환경영향을 평가하였다. 그 결과 낙진량은 기본적으로 분진원으로부터 거리가 멀어질 수록 현저하게 감소하며, 같은 조건일 때는 풍속이 빠를수록 낙진량도 증가하였다. 또한 석회석 노천채광시 발파작업장으로부터 100m 내외의 주변 지표상의 낙진량은 아주 작은량임을 알 수 있었다.

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요트세일의 풍동시험을 위한 공력 계측시스템 구축과 모형세일의 공력 계측 (A Construction of Aerodynamic Force Measurement System for Wind Tunnel Test of Yacht Sail and Aerodynamic Forces Measurement of Model Sail)

  • 김철희;최정규;김형태
    • 대한조선학회논문집
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    • 제48권5호
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    • pp.445-450
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    • 2011
  • In order to estimate a yacht sail performance, measuring system of aerodynamic forces acting on the yacht sail is constructed and experiments of flexible model sail are carried out at the medium-size subsonic wind tunnel of Chungnam National University. Experimental results for a flexible sail are compared with experimental and numerical results of fixed shape sail. In case of a fixed shape sail, lift and drag coefficients are rarely changed at all velocity conditions. However, those of the flexible sail are decreased as the incoming velocity is increased. These are understandably resulted from shape variations due to the flexible material. Therefore aero-elastic similarity should be more carefully considered in the model test rather than other similarities.

풍동을 이용한 고속철의 차간 공간에서의 공력 소음 측정 및 특성 분석 (Wind tunnel tests for analyzing noise generation from the inter-coach spacing of a high-speed train)

  • 박기형;송시몬;김태호;이택진;최성훈;박준홍
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 추계학술대회논문집
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    • pp.65-68
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    • 2006
  • Experiments were performed to investigate the effects of mud-flap width on the aeroacoustic noise generation inside high-speed trains. The open-circuit type wind tunnel was used. The measurement setup was custom-built to simulate intercoach spacing. From the measurements, the characteristics of the turbulent flow after the intercoach spacing and consequent generation of aeroacoustic noise inside the cabin was investigated. Especially the effects of mud flap length on the characteristics of the characteristics of the turbulent flow were identified. The mechanism of noise generation by analyzed interactions with structure vibration characteristics and generation characteristics of blocked pressure was investigated.

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