• 제목/요약/키워드: aerodynamic measure

검색결과 112건 처리시간 0.027초

스텔스 형상 공력특성에 관한 실험적 연구 (An Experimental Study on the Aerodynamic Characteristics of a Stealth Configuration)

  • 오세윤;김상호;안승기;조철영;이종건
    • 한국항공우주학회지
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    • 제36권10호
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    • pp.962-968
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    • 2008
  • 국방과학연구소 풍동실험실에서는 스텔스 형상 무인전투기개발에 필요한 공력특성 측정과 관련시험기법의 확립을 위한 실험적 연구를 수행하였다. 본 연구에서는 스텔스 특성을 가진 형상의 공기역학적 특성의 추출과 5-hole probe를 이용한 유동장 특성의 측정을 목적으로 하였으며, 시험결과들의 분석과 앞전 형상의 변경에 따른 공력특성의 변화도 함께 고찰하였다.

다양한 조건의 저압 공정 모니터링을 위한 입자 집속 장치 개발 (Development of particle focusing device to monitor various low pressure processes)

  • 김명준;김동빈;강상우;김태성
    • 한국입자에어로졸학회지
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    • 제13권2호
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    • pp.53-63
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    • 2017
  • As semiconductor process was highly integrated, particle contamination became a major issue. Because particle contamination is related with process yields directly, particles with a diameter larger than half pitch of gate should be controlled. PBMS (Particle beam mass spectrometry) is one of powerful nano particle measurement device. It can measure 5~500 nm particles at ~ 100 mtorr condition in real time by in-situ method. However its usage is restricted to research filed only, due to its big device volume and high price. Therefore aperture changeable aerodynamic lenses (ACALs) which can control particle focusing characteristics by changing its aperture diameter was proposed in this study. Unlike conventional aerodynamic lenses which changes particle focusing efficiency when operating condition is changed, ACALs can maintain particle focusing efficiency. Therefore, it can be used for a multi-monitoring system that connects one PBMS and several process chambers, which greatly improves the commercialization possibility of the PBMS. ACALs was designed based on Stokes number and evaluated by numerical method. Numerical analysis results showed aperture diameter changeable aerodynamic lenses can focus 5 to 100 nm standard particles at 0.1 to 10 torr upstream pressure.

공력 저항 측정기를 이용한 방풍펜스 방진막의 공기 투과 저항력 측정 (Measurement of Aerodynamic Properties of Screens for Windbreak Fence using the Apparatus for Testing Screens)

  • 김락우;이인복;홍세운;황현섭;손영환;김태완;김민영;송인홍
    • 한국농공학회논문집
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    • 제55권6호
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    • pp.145-154
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    • 2013
  • Recently, damage occurrence by wind erosion has been increasing in society. In times past, such problems only took place in desert area ; however, in recent years, the wind erosion problem is spreading out to agricultural land. Wind erosion in agricultural land can cause loss of loam soils, the disturbance of the photosynthesis of the crop fields and serious economic losses. To overcome the mentioned problems, installation of windbreak fence can be recommended which function as disturbing strong wind and wind erosion. However, there is still no proper guideline to install the windbreak fence and the installation used to rely on the intuition of the workers due to the lack of related studies. Therefore, this study measured the aerodynamic resistance of screens of the windbreak fence using the apparatus for testing screens. The apparatus for testing screens was designed to measure pressure loss around the screen. Measured pressure loss by wall friction compensated for pressure loss to calculate the aerodynamic resistance of screens. The result of pressure loss by regression analysis derived the aerodynamic coefficient of Darcy-Forchheimer equation and power law equation. The aerodynamic resistance was constant regardless of the overlapped shape when the screen was overlapped into several layers. Increasing the number of layers of the screen, internal resistance increased significantly more, and pressure loss caused by the screen also increased linearly when the wind speed was certain conditions, but permeability had no tendency. In the future, the results of this study will be applied to the computational fluid dynamics simulation. The simulation models will be also validated in advance by wind tunnel experiments. It will provide standard of a design for constructing windbreak fence.

유사측도를 이용한 무인기의 고장진단 및 검출 (Fault Detection and Identification of Uninhabited Aerial Vehicle using Similarity Measure)

  • 박욱제;이상혁
    • 한국항공운항학회지
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    • 제19권2호
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    • pp.16-22
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    • 2011
  • It is recognized that the control surface fault is detected by monitoring the value of the coefficients due to the control surface deviation. It is found out the control surface stuck position by comparing the trim value with the reference value. To detect and isolate the fault, two mixed methods apply to the real-time parameter estimation and similarity measure. If the scatter of aerodynamic coefficients for the fault and normal are closing nearly, fault decision is difficult. Applying similarity measure to decide for fault or not, it makes a clear and easy distinction between fault and normal. Low power processor is applied to the real-time parameter estimator and computation of similarity measure.

Wind loads on a moving vehicle-bridge deck system by wind-tunnel model test

  • Li, Yongle;Hu, Peng;Xu, You-Lin;Zhang, Mingjin;Liao, Haili
    • Wind and Structures
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    • 제19권2호
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    • pp.145-167
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    • 2014
  • Wind-vehicle-bridge (WVB) interaction can be regarded as a coupled vibration system. Aerodynamic forces and moment on vehicles and bridge decks play an important role in the vibration analysis of the coupled WVB system. High-speed vehicle motion has certain effects on the aerodynamic characteristics of a vehicle-bridge system under crosswinds, but it is not taken into account in most previous studies. In this study, a new testing system with a moving vehicle model was developed to directly measure the aerodynamic forces and moment on the vehicle and bridge deck when the vehicle model moved on the bridge deck under crosswinds in a large wind tunnel. The testing system, with a total length of 18.0 m, consisted of three main parts: vehicle-bridge model system, motion system and signal measuring system. The wind speed, vehicle speed, test objects and relative position of the vehicle to the bridge deck could be easily altered for different test cases. The aerodynamic forces and moment on the moving vehicle and bridge deck were measured utilizing the new testing system. The effects of the vehicle speed, wind yaw angle, rail track position and vehicle type on the aerodynamic characteristics of the vehicle and bridge deck were investigated. In addition, a data processing method was proposed according to the characteristics of the dynamic testing signals to determine the variations of aerodynamic forces and moment on the moving vehicle and bridge deck. Three-car and single-car models were employed as the moving rail vehicle model and road vehicle model, respectively. The results indicate that the drag and lift coefficients of the vehicle tend to increase with the increase of the vehicle speed and the decrease of the resultant wind yaw angle and that the vehicle speed has more significant effect on the aerodynamic coefficients of the single-car model than on those of the three-car model. This study also reveals that the aerodynamic coefficients of the vehicle and bridge deck are strongly influenced by the rail track positions, while the aerodynamic coefficients of the bridge deck are insensitive to the vehicle speed or resultant wind yaw angle.

A Study on the Measurement of Contact Force of Pantograph on High Speed Train

  • Seo, Sung-Il;Cho, Yong-Hyun;Mok, Jin-Yong;Park, Choon-Soo;Kim, Ki-Hwan
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.1374-1378
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    • 2005
  • Appropriate upward force is crucial for the pantograph on high speed train to collect current from the catenery system without separation. However, at high speed, large aerodynamic lifting force is generated by the contact plate and the arms of pantograph, which may cause wear of the contact wire. In this study, to confirm the interface performance of the pantograph on Korea High Speed Train, a method to measure the contact force of the pantograph was proposed and the related measurement system was developed. The forces acting on the pantograph were clarified and a procedure to calculate the aerodynamic lifting force was proposed. A special device was invented and applied to measure the lifting force. Measured contact forces were displayed by the developed system and evaluated according to the criteria. Countermeasures were also taken to reduce the contact force based on the results.

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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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풍동실험을 통한 사장교의 내풍 안전성 검토 (Wind-Resistant Safety Reviews of Cable-Stayed Bridge by Wind Tunnel Tests)

  • 허택녕
    • 한국산업융합학회 논문집
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    • 제23권4_2호
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    • pp.637-644
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    • 2020
  • Because suicide accidents sometimes were happened in grand bridges over rivers or sea water recently, it will be necessary that prevention measures be made preparation in advance from now on. Additional safety facilities must be needed in addition to existing safety facilities in such a way as this prevention measure. In order to make cable-stayed bridge safe on wind for additional safety facilities, main girder models with added safety facilities for wind-tunnel tests was made, and wind tunnel experiments was carried out to measure aerodynamic force coefficients. Also, wind-resistant analyses of 3D cable-stayed bridge were performed on the basis of wind-tunnel test results. From the wind experiments, force coefficients of main girder with added safety facilities were assessed, and it is known that there are little possibility of galloping and rotation of steel main girder. Finally, from the wind resistant analyses, it was concluded that wind-resistant safety of cable-stayed bridge was secured on wind speed 60.6m/sec.

Phonation Threshold Flow and Phonation Threshold Pressure in Patients with Adductor Spasmodic Dysphonia

  • Choi, Seong-Hee;Jiang, Jack J.;Yun, Bo-Ram;Lee, Ji-Yeoun;Lim, Sung-Eun;Choi, Hong-Shik
    • 말소리와 음성과학
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    • 제2권3호
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    • pp.157-164
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    • 2010
  • This study investigated the characteristics of two aerodynamic indices, PTP (Phonation threshold pressure) and PTF (Phonation threshold flow) in patients with ADSD (adductor spasmodic dysphonia) and to see if two new aerodynamic indices can differentiate between normal and ADSD group. Additionally, PTP and PTF values were compared in terms of overall severity of ADSD in the patient group. The severity of ADSD was rated on a 7-point rating scale by two experienced speech language pathologists. The Kay Elemetrics Phonatory Aerodynamic System (PAS) (Kay Elemetrics Corp., Lincoln Park, NJ) was used to collect PTP and PTF measurements from 16 female normal subjects, 31 female patients with ADSD. Significantly lower PTF values (P< 0.05) were observed in ADSD when compared to those of normal control. Also, significantly lower PTF values in severe ADSD patients (P<.001). However, PTP could not distinguish patients with ADSD from control groups (P=0.119) and among the ADSD groups according to the severity (P=0.177). Consequently, PTF was more sensitive than PTP which might differentiate between normal speakers and ADSD and among different levels of severity within ADSD, suggesting that PTF could be a useful diagnostic parameter to measure the aerodynamic function of ADSD and provide the neurolaryngeal dysfunction in patients with ADSD.

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고속철도차량의 공력소음 측정 시험법 개발 (Development of aerodynamic noise measurement method for high-speed trains)

  • 정민승;김재환;장형석;김종환;정철웅;이권기
    • 한국음향학회지
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    • 제43권1호
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    • pp.131-137
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    • 2024
  • 고속으로 주행하는 열차의 주변 유동에 의해 발생하는 공력소음은 실외소음과 실내소음에 모두 영향을 미친다. 본 연구는 열차표면의 압력섭동데이터를 통해 공력소음을 측정하고 실내소음에 영향을 미치는 성분을 정량적으로 평가하기 위한 시험법을 개발하고 분석하는 것이다. 실내소음을 정확히 평가하기 위해서는 취득한 표면 압력섭동 데이터에서 혼재되어 있는 압축성 압력섭동과 비압축성 압력섭동을 각각 분리하여 평가하는 것이 중요하다. 이는 두 압력섭동의 소음 전달 특성이 다르기 때문이다. 먼저 마이크로폰의 설치 길이와 간격을 결정하여 표면 압력섭동 데이터를 취득하였고, 파수-주파수 분석을 수행하여 비압축성 압력섭동과 압축성 압력섭동을 분리하여 음압 스펙트럼을 취득하였다. 마지막으로 전두부와 후두부에서 측정한 시험 결과값을 비교한 결과 전두부 표면 압력섭동이 후두부 압력섭동보다 더 큼을 확인하였다.