• 제목/요약/키워드: High speed wind tunnel test

검색결과 99건 처리시간 0.027초

Dynamic analysis of wind-vehicle-bridge system considering additional moments of non-uniform winds by wind shielding effect of multi-limb tower

  • Xu Han;Huoyue Xiang;Xuli Chen;Yongle Li
    • Wind and Structures
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    • 제36권1호
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    • pp.1-14
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    • 2023
  • To evaluate the wind shielding effect of bridge towers with multiple limbs on high-speed trains, a wind tunnel test was conducted to investigate the aerodynamic characteristics of vehicles traversing multi-limb towers, which represented a combination of the steady aerodynamic coefficient of the vehicle-bridge system and wind environment around the tower. Subsequently, the analysis model of wind-vehicle-bridge (WVB) system considering the additional moments caused by lift and drag forces under nonuniform wind was proposed, and the reliability and accuracy of the proposed model of WVB system were verified using another model. Finally, the factors influencing the wind shielding effect of multi-limb towers were analyzed. The results indicate that the wind speed distributions along the span exhibit two sudden changes, and the wind speed generally decreases with increasing wind direction angle. The pitching and yawing accelerations of vehicles under nonuniform wind loads significantly increase due to the additional pitching and yawing moments. The sudden change values of the lateral and yawing accelerations caused by the wind shielding effect of multi-limb tower are 0.43 m/s2 and 0.11 rad/s2 within 0.4 s, respectively. The results indicate that the wind shielding effect of a multi-limb tower is the controlling factor in WVB systems.

로켓 부스터 분리 고속 풍동시험 (High-Speed Wind Tunnel Test on Rocket Booster Separation)

  • 라승호;김인선;옥호남;오범석;이준호
    • 한국항공우주학회지
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    • 제33권10호
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    • pp.75-81
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    • 2005
  • 낙하물 및 로켓 단분리 등과 같은 비행체 분리물의 궤적을 모사하기 위해 사출, 격자 및 CTS 시험과 같은 풍동시험 기법이 많이 사용된다. 본 논문에서는 3단형 과학로켓 개발 시 사용된 격자 및 CTS 시험 기법 및 대표적인 결과를 소개하였다. 시험에 사용된 풍동은 ONERA S2MA이며 마하수 2.0과 2.8에 대해 13개의 분리 궤적을 시험하였다. 시험 결과는 분리장치를 최적화기 위한 데이터베이스로 활용되었다.

회전발사체 롤댐핑 특성에 관한 고속 유동장 실험연구 (An Experimental Study on Roll-Damping Characteristics of a Spinning Projectile at High Speed Region)

  • 오세윤;이도관;김성철;김상호;안승기
    • 한국항공우주학회지
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    • 제39권10호
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    • pp.912-918
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    • 2011
  • 본 연구의 목적은 풍동실험을 통해 회전발사체에서 발생하는 동적 롤댐핑 특성을 실험적으로 측정하는데 있었으며, 이를 위해 약 12,000 rpm으로 회전하는 회전발사체 실험모형에 작용하는 롤댐핑 특성의 측정을 위한 고속풍동실험을 국방과학연구소 삼중음속풍동에서 수행하였다. 실험시의 마하수는 0.7~1.05까지의 천음속 영역이었으며 이때의 받음각 구간은 -4~+10 deg이었다. 풍동실험 측정기법의 유효성 평가를 위해 동일형상 모형에 대해 기 수행하였던 롤댐핑 측정결과와의 비교검토를 수행하였다.

수직형 풍동을 응용한 고공강하 시뮬레이터의 설계에 대한 연구 (A Study on the Design of Free-Fall Simulator using concept of Vertical Wind Tunnel)

  • 최상길;조진수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.447-452
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    • 2000
  • In this study, the design of Free-Fall Simulator was carried out using concept of vertical wind tunnel. Free-Fall Simulator is not an experimental equipment but a training equipment. Therefore Free-Fall Simulator needs a large training section compared with test section of wind tunnel and has critical limit of height. These limits bring about the difficulty of design for a return passage. Due to small area ratio, the downstream flow of training section with high speed is not decelerated adequately to the fan section. High-speed flow leads to great losses in the small area ratio diffuser and corner. So design of diffusers and corners located between training section and fan section has a great effect on the Free-Fall Simulator performance. This study used an estimation method of subsonic wind tunnel performance. It considered each section of Free-Fall Simulator as an independent section. Therefore loss of one section didn't affect loss of other sections. Because losses of corner with vane and $1^{st}$ diffuser are most parts of overall Free-Fall Simulator, this study focused on the design of these sections.

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고속철도 판토그래프의 공력소음 기여도 연구 (Prediction of the Aerodynamic Noise Generated by Pantograph on High Speed Trains)

  • 한재현;김태민;김정태
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 춘계학술대회 논문집
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    • pp.425-431
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    • 2013
  • Nowadays, high speed train has settled down as a fast and convenient environment-friendly transportation and it's need is gradually increasing. However increased train speed leads to increased aerodynamic noise, which causes critically affects comfortability of passengers. Especially, the pantograph of high speed train is protruded out of train body, which is the main factor for increased aerodynamic noise. Since aerodynamic noise caused pantograph should be measured in high speed, it is difficult to measure it and to analysis aerodynamic noise characteristics due to the various types of pantograph. In this research, aerodynamic noise of pantograph is predicted by CFD (Computational Fluid Dynamic) and FW-H (Ffowcs Williams-Hawkings) equation. Also, Wind tunnel test results and numerical simulation results were compared. As a result, Simulation results predicting sound pressure level is very similar with wind tunnel test result. To analyze contribution of the pantograph to the noise of high-speed train, simulation results compared with measurement results of exterior noise. The simulation reuslts found that pantograph is a dominant noise source of high-speed trains's exterior noise in low frequency section. This dominant noise was come out from vortex shedding of the panhead in the pantograph. This research will be utilized for reduce sound pressure level of pantograph.

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Wind load parameters and performance of an integral steel platform scaffold system

  • Zhenyu Yang;Qiang Xie;Yue Li;Chang He
    • Wind and Structures
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    • 제36권4호
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    • pp.263-275
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    • 2023
  • As a new kind of construction facility for high rise buildings, the integral steel platform scaffold system (ISPS) consisting of the steel skeleton and suspended scaffold faces high wind during the construction procedure. The lattice structure type and existence of core tubes both make it difficult to estimate the wind load and calculate the wind-induced responses. In this study, an aeroelastic model with a geometry scale ratio of 1:25 based on the ISPS for Shanghai Tower, with the representative square profile, is manufactured and then tested in a wind tunnel. The first mode of the prototype ISPS is a torsional one with a frequency of only 0.68 Hz, and the model survives under extreme wind speed up to 50 m/s. The static wind load and wind vibration factors are derived based on the test result and supplementary finite element analysis, offering a reference for the following ISPS design. The spacer at the bottom of the suspended scaffold is suggested to be long enough to touch the core tube in the initial status to prevent the collision. Besides, aerodynamic wind loads and cross-wind loads are suggested to be included in the structural design of the ISPS.

Field monitoring of wind effects on a super-tall building during typhoons

  • Zhi, Lunhai;Li, Q.S.;Wu, J.R.;Li, Z.N.
    • Wind and Structures
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    • 제14권3호
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    • pp.253-283
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    • 2011
  • This paper presents the field measurement results of wind effects on a super-tall building (CITIC Plaza, 391 m high) located in Guangzhou. The field data such as wind speed, wind direction and acceleration responses were simultaneously and continuously recorded from the tall building by a wind and vibration monitoring system during two typhoons. The typhoon-generated wind characteristics including turbulence intensity, gust factor, peak factor, turbulence integral length scale and power spectral density of fluctuating wind speed were presented and discussed. The dynamic characteristics of the tall building were determined based on the field measurements and compared with those calculated from a 3D finite element model of the building. The measured natural frequencies of the two fundamental sway modes of the building were found to be larger than those calculated. The damping ratios of the building were evaluated by the random decrement technique, which demonstrated amplitude-dependent characteristics. The field measured acceleration responses were compared with wind tunnel test results, which were found to be consistent with the model test data. Finally, the serviceability performance of the super-tall building was assessed based on the field measurement results.

Design criteria of wind barriers for traffic -Part 1: wind barrier performance

  • Kwon, Soon-Duck;Kim, Dong Hyawn;Lee, Seung Ho;Song, Ho Sung
    • Wind and Structures
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    • 제14권1호
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    • pp.55-70
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    • 2011
  • This study investigates the design criteria required for wind barriers to protect vehicles running on an expressway under a high side wind. At the first stage of this study, the lateral deviations of vehicles in crosswinds were computed from the commercial software, CarSim and TruckSim, and the critical wind speeds for a car accident were then evaluated from a predefined car accident index. The critical wind speeds for driving stability were found to be 35 m/s for a small passenger car, yet 30 m/s for a truck and a bus. From the wind tunnel tests, the minimum height of a wind barrier required to reduce the wind speed by 50% was found to be 12.5% of the road width. In the case of parallel bridges, the placement of two edge wind barriers plus one wind barrier at center was recommended for a separation distance larger than 20 m (four lanes) and 10 m (six lanes) respectively, otherwise two wind barriers were recommended.

전투기급 항공기 초음속 순항 성능에 미치는 앞전플랩 변위 효과 (The Effects of Leading Edge Flap Deflection on Supersonic Cruise Performance of a Fighter Class Aircraft)

  • 정인재;김상진;김명성
    • 한국항공우주학회지
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    • 제35권10호
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    • pp.899-904
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    • 2007
  • 전투기급 항공기 개념설계 기간 중 항공기 초음속 순항성능에 미치는 앞전플랩 굽힘 효과를 분석하기 위하여 1/20 축척 날개-동체-꼬리 형상 모형을 사용한 고속 풍동시험을 수행하였다. 풍동시험을 위한 적절한 앞전플랩 각도를 선정하기 위하여 보정된 초음속 패널 방법을 사용하여 다양한 앞전플랩 굽힘 각도에 따른 공력특성을 분석하였다. 실험 및 수치해석적 접근 결과 분석을 기초로, 앞전플랩 굽힘 효과는 전투기급 항공기의 초음속 순항 성능 증대에 유용한 것으로 확인되었다.

Wind characteristics in the high-altitude difference at bridge site by wind tunnel tests

  • Zhang, Mingjin;Zhang, Jinxiang;Li, Yongle;Yu, Jisheng;Zhang, Jingyu;Wu, Lianhuo
    • Wind and Structures
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    • 제30권6호
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    • pp.547-558
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    • 2020
  • With the development of economy and construction technology, more and more bridges are built in complex mountainous areas. Accurate assessment of wind parameters is important in bridge construction at complex terrain. In order to investigate the wind characteristics in the high-altitude difference area, a complex mountain terrain model with the scale of 1:2000 was built. By using the method of wind tunnel tests, the study of wind characteristics including mean wind characteristics and turbulence characteristics was carried out. The results show: The wind direction is affected significant by the topography, the dominant wind direction is usually parallel to the river. Due to the sheltering effect of the mountain near the bridge, the wind speed and wind attack angle along the bridge are both uneven which is different from that at flat terrain. In addition, different from flat terrain, the wind attack angle is mostly negative. The wind profiles obey exponential law and logarithmic law. And the fitting coefficient is consistent with the code which means that it is feasible to use the method of wind tunnel test to simulate complex terrain. As for turbulence characteristics, the turbulence intensity is also related to the topography. Increases sheltering effect of mountain increases the degree of breaking up the large-scale vortices, thereby increasing the turbulence intensity. Also, the value of turbulence intensity ratio is different from the recommended values in the code. The conclusions of this study can provide basis for further wind resistance design of the bridge.