• 제목/요약/키워드: wind tunnel experiments

검색결과 226건 처리시간 0.025초

지면효과익의 공기역학특성을 위한 모사실험장치 개발에 관한 연구 (Simulator Development for the Aerodynamic Characteristics of a Wing in Ground)

  • 김태호;김희동;이명호;손명환;촌수남
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.1724-1729
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    • 2003
  • A new ground transportation system is often simulated by the wing in ground effect(WIG). Recently, several kinds of experimental and computational studies are being carried out to investigate the WIG aerodynamic characteristics which are of practical importance to develop the new ground transportation vehicle system. These works are mainly based on conventional wind tunnel tests, but many problems associated with the WIG aerodynamic characteristics can not be satisfactorily resolved. In order to develop the new ground transportation vehicle system the WIG should be further investigated. To do this, it is necessary to develop a s imulator appropriate to the WIG aerodynamics. The objective of the present study is to clarify the aerodynamic characteristics of the WIG and to develop a new experimental test rig for the investigation of the WIG aerodynamics. Some preliminary experiments are performed to investigate the usefulness of the WIG simulator.

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선형터빈 케스케이드 통로내의 2차 유동과 손실에 관한 연구 (The Experimental Investigation of the Secondary Flow and Losses Within the Plane Turbine Cascade Passage)

  • 이기백;양장식;나종문
    • 대한기계학회논문집
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    • 제19권3호
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    • pp.784-795
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    • 1995
  • This paper represents the results of the experiments of the three-dimensional flow and the aerodynamic loss caused by the three-dimensional flow within the plane bucket blades. To research the secondary flow and the aerodynamic loss, the large-scale plane bucket blade of lst-stage in the low pressure steam turbine is made of FRP. The detailed investigation of the secondary flow and the aerodynamic loss using 5-hole pressure probe within turbine cascade has been carried out in the low speed wind tunnel. The limiting streamlines of the suction and endwall surface have been visualized by the oil film method. The flow visualization of the secondary flow has been performed by the laser light sheet technique and image processing system. By using the method mentioned above, it is possible to observe the evolution of the pitchwise mass-averaged flow deviation angle and total pressure loss coefficient, the secondary flow, and the aerodynamic loss through the cascade.

동력 철도차량 기관실의 효과적인 환기에 관한 실험적 연구 (Experiments on the Effective Engine Room Ventilation in a Power Car)

  • 한석윤;이진호
    • 설비공학논문집
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    • 제2권3호
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    • pp.166-176
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    • 1990
  • Experimental study was made to find the effective ways for cooling of engine room in a power car through natural ventilation, forced ventilation and wind tunnel test of 1:10 model. Through the measurements of inner temperature of engine room and pressure distribution of model surface for the various opening combinations and the fan locations, the following results are obtained. For natural ventilation, side and top opening combination is more effective than the side openings only and optimal opening combination is all side openings with top center opening. For forced ventilation with fan on the roof, the combination of all sides and top opening is more effective than the combination of side and top opening, and the optimal location of fan is top center. When the model is located in the air stream, the combination of side and top opening is more effective than the side openings only, and the optimal location of top opening is the front opening. With both air stream and forced ventilation, the optimal location of fan is the side region, and the direction of side grill installation is found to have negligible effect on the room ventilation.

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MEMS 기반의 차량용 휨형 유속센서의 제작 및 특성 연구 (Study on the Fabrication and Evaluation of the MEMS Based Curved Beam Air Flowmeter for the Vehicle Applications)

  • 박철민;최대근;이상훈
    • 센서학회지
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    • 제25권2호
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    • pp.116-123
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    • 2016
  • This paper presents the fabrication and evaluation of the novel drag force type air flowmeter using MEMS technologies for the vehicle applications. To obtain the air drag force, the flowmeter utilized the curved beam structure, which was realized by the difference of residual stress between the silicon oxide layer and the silicon nitride layer. The paddle structure was applied for the maximum air drag force, and the dual-beam was adapted to prevent distortion. The basic experiments were performed in the wind tunnel, and the stable outputs were obtained. The device was applied to the internal combustion engine, and the results were compared with the HI-DS output where the convection thermal flowmeter was used as the reference sensor. The results indicated that the comparable resolutions and response times were obtained under the various engine speeds.

이동하는 소음원 위치 추정을 위한 다양한 빔형성 기법 적용 (Localization of Moving Sound Source Using Various Beamforming Methods)

  • 고영주;이재형;최종수;하재현
    • 한국소음진동공학회논문집
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    • 제26권5호
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    • pp.501-510
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    • 2016
  • Capabilities of several beamforming techniques are compared for estimating the position of a moving source. Beamforming has enabled to widen our perspective of aeroacoustics in wind tunnel experiments and has provided useful approach in array measurements. Meanwhile beamforming techniques have been developed in a way to improve estimation accuracy and to save ing effort at the same time. In order to achieve reasonable outcome from aeroacoustic measurement, it is important to identify the spectral characteristics of source and to select an appropriate beamformer. Though aeroacoustic sources normally generates broadband noises, many array signal processing have been focused on narrowband processing which makes calculation numerically efficient. However, calculation in frequency-domain requires selection of single frequency of interest which affects spatial resolution and sidelobe level as a consequence. To be able to localize broadband noise source, it is proposed to use broadband beamforming. The formulas implements the deletion of diagonal term from cross spectral matrix. In this study, trajectory of flying source emitting broadband noise was simulated and several beamformers are applied.

초소형 관성측정모듈을 이용한 플라잉디스크의 수평축 모멘트 미계수 추정 연구 (A Study on Horizontal Moment Flight Coefficient Estimation of a Flying Disc Using Miniaturized Inertial Measurement Module)

  • 손현진;이주환;이영재;성상경
    • 한국항공우주학회지
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    • 제46권5호
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    • pp.385-392
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    • 2018
  • 본 논문은 플라잉디스크에 탑재된 계측모듈의 IMU 데이터를 이용하여 롤링 및 피칭모멘트 감쇠미계수를 추정하는 방식을 새롭게 제시한다. 제안한 방식은 반복된 수 회의 원반 비행 실험을 수행하여 데이터를 구축한 뒤 공력 계수를 추정하므로, 풍동이나 전산유체해석을 이용하는 방법에 비해 수월한 실험적 대안이 될 수 있다. 추정한 공력 계수는 플라잉디스크의 비행동역학 모델을 토대로 구현한 시뮬레이터에 적용하여 비행 궤적을 예측하는 것에 이용되었으며, 이를 GPS의 위치 궤적과 비교함으로써 성능을 검증하였다.

조개 표면의 종방향 그루브가 공력성능에 미치는 영향 (Effect of longitudinal grooves of the scallop surface on aerodynamic performance)

  • 김태훈;최해천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2419-2421
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    • 2008
  • Some of the scallops like Amesium balloti have an excellent level-swimming ability, i.e. they can swim about 20m by single level swimming with a maximum swimming velocity of about 1.6m/s in the sea. On the other hand, some species like Patinopecten yessoensis have longitudinal grooves on the upper and lower surfaces and others do not. Therefore, in the present study, we measure the lift and drag forces on a real scallop model (Patinopecten yessoensis) in a wind tunnel. Experiments are performed at the Reynolds number of 75,000 based on the maximum chord length, which is within the swimming condition of real scallop (Re = $30,000{\sim}300,000$). To see the effect of longitudinal grooves, we measure the aerodynamic forces on a scallop model by removing the grooves. With the grooves, the lift force increases at low angles of attack (${\alpha}<10^{\circ}$). The drag force increases slightly at all the attack angles considered. The lift-to-drag ratio is increased by about 10% at ${\alpha}<10^{\circ}$.

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원심형 송풍기의 날개 특성에 따른 성능에 관한 연구 (A Study on the Performance of Centrifugal Blowers by Blades Characteristics)

  • 김재원;안은영
    • 한국유체기계학회 논문집
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    • 제7권5호
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    • pp.13-19
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    • 2004
  • Centrifugal blowers are widely used for air handling units in industry applications. The blower has a centrifugal impeller and a scroll casing including a driving component such as an electric motor. The impeller takes forward or backward blades to induce flows into the blower, Comprehensive investigation according to the two kinds of blades is systematically carried out for a guidance of design for this kind research. It is observed that flow rate of the blower with forward blades is larger than that of the system with backward blades. Otherwise, the system noise is more pronounced in the case of the blower with forward blades. The reason is due to larger velocity from the rotating forward blades that pose obtuse angle with the circumferential direction. The distinguished characteristics are validated by a parallel experiments with a wind tunnel and in an anechoic chamber. Numerical analysis for the system shows detail information inside the blades and the casing. A series of figures to show the flow details offer deep understanding of the performance of a centrifugal blower with different blades.

와동 발생기를 이용한 자외선 살균 시스템 성능 향상에 관한 연구 (A Study on Enhancement of UV Disinfection System Performance by the Vortex Generator)

  • 김봉환;안국찬;김동진
    • 한국안전학회지
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    • 제22권1호
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    • pp.24-29
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    • 2007
  • The effectiveness of a UV(ultra violet) disinfection system depends on the characteristics of the waste water, flow conditions, the intensity of UV radiation, the amount of time the microorganisms are exposed to the radiation, and the reactor configuration. The wast water flow conditions are important factors in the design of UV disinfection system from the point of enhancement view of UV disinfection. The turbulent energy intensity in the wake by the vortex shedding are effective for UV radiation. Therewith the effectiveness of vortex generator is considered as a enhancement of UV disinfection. The experimental results presented give important evidences and explain that it is possible to predict UV disinfection performance based on flow experiments. An experimental investigation of two types of the vortex generator is presented. The qualitative and quantitative evaluations of the wake are made by flow visualization using smoke wire method and the measurement of vortex frequencies in the wind tunnel. From the experiment, following results were obtained that the delta wing type vortex generator is more effective than circular type because of the higher vortex frequencies and the smaller drag.

Characteristics of Droplet Properties in the Two-Phase Spray into a Subsonic Cross Flow

  • Lee, I.C.;Cho, W.J.;Koo, J.Y.
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.358-363
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    • 2008
  • The spray cross-section characteristics of two-phase spray that using external-mixing nozzle injected into a subsonic cross flow were experimentally studied with various ALR ratio that is $0{\sim}59.4%$. Suction type wind tunnel was used and experiments were conducted to ambient environment. Several plain orifice nozzles with L/d of 30 and orifice diameter of 0.5 mm and orifice length 1.5 mm were tested. Free stream velocity profiles at the injection location were measured using hot wire. Spray images were captured to study collision point and column trajectory. Phase Doppler particle analyzer(PDPA) was utilized to quantitatively measuring droplet SMD, volume flux. Measuring probe of PDPA positions was moved 3-way transverse machine. SMD distributions were layered structure and peaked at the top of the spray plume and low value at bottom of the spray. Volume flux of spray was distributed to the two side region and volume flux quantity decreased when ALR ratio increased. It was found that the perpendicularly injected two-phase spray jet of external mixing into a cross flow showing that mistlike spray moved away from the test section bottom region.

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