• Title/Summary/Keyword: Gust

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유연날개 돌풍응답경감제어를 위한 서보공탄성 모델링 및 돌풍응답해석 (Aeroservoelastic Modeling and Gust Response Analysis of Flexible Wing for Gust Response Alleviation)

  • 김성찬;홍창호
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2010년도 정기 학술대회
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    • pp.488-491
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    • 2010
  • 본 논문에서는 돌풍응답경감제어 효과 검증을 위한 풍동시험에 사용될 유연날개에 대해 공탄성 모델, 조종면 작동기 모델, 돌풍 모델 등으로 구성되는 서보공탄성 모델링을 수행하였으며, 이에 대한 연속돌풍 응답해석을 수행하여 상용 Solver를 이용한 해석결과와 비교하여 구성된 서보공탄성 모델을 검증하였다. 또한, 유연날개의 돌풍응답을 경감하는 조종면 제어기를 설계하고, 이에 대한 수치 시뮬레이션을 수행하여 돌풍응답 경감효과를 검증하였다.

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Computer Simulation of a Train Exiting a Tunnel through a Varying Crosswind

  • Krajnovic, S.
    • International Journal of Railway
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    • 제1권3호
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    • pp.99-105
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    • 2008
  • Flow around an ICE2 high-speed train exiting a tunnel under the influence of a wind gust has been studied using numerical technique called detached eddy simulation. A wind gust boundary condition was derived to approximate previous experimental observations. The body of the train includes most important details including bogies, plugs, inter-car gaps and rotating wheels on the rail. The maximal yawing and rolling moments which possibly can cause a derailment or overturning were found to occur when approximately one third and one half of the train, respectively, has left the tunnel. These are explained by development of a strong vortex trailing along the upper leeward edge of the train. All aerodynamic forces and moments were monitored during the simulation and the underlying flow structures and mechanisms are explained.

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주기적으로 거동하는 유동장의 인공 초월공동에 대한 실험연구 (Experimental Investigation of Artificial Supercavitation under Periodic Gust Flows)

  • 정소원;박상태;안병권
    • 한국군사과학기술학회지
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    • 제21권2호
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    • pp.188-194
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    • 2018
  • Recently a supercavitating underwater vehicle moving at high speed over 200 knots has been of interest for its practical advantage of the dramatic drag reduction. Many experimental and numerical studies have been explored, however most of the studies deal with the case of uniform flows. In this paper, we investigated physical behaviors of the artificial supercavity in a periodic gust flow. Experiments were carried out at a cavitation tunnel of the Chungnam National University(CNUCT), which is equipped to remove the gas supplied from outside of the tunnel. We devised an experimental apparatus generating vertical and horizontal gust flows, and investigated the supercavity formations at different periodic mode of the incoming flow.

Aeroelastic tailoring using crenellated skins-modelling and experiment

  • Francois, Guillaume;Cooper, Jonathan E.;Weaver, Paul M.
    • Advances in aircraft and spacecraft science
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    • 제4권2호
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    • pp.93-124
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    • 2017
  • Aeroelastic performance controls wing shape in flight and its behaviour under manoeuvre and gust loads. Controlling the wing‟s aeroelastic performance can therefore offer weight and fuel savings. In this paper, the rib orientation and the crenellated skin concept are used to control wing deformation under aerodynamic load. The impact of varying the rib/crenellation orientation, the crenellation width and thickness on the tip twist, tip displacement, natural frequencies, flutter speed and gust response are investigated. Various wind-off and wind-on loads are considered through Finite Element modelling and experiments, using wings manufactured through polyamide laser sintering. It is shown that it is possible to influence the aeroelastic behaviour using the rib and crenellation orientation, e.g., flutter speed increased by up to 14.2% and gust loads alleviated by up to 6.4%. A reasonable comparison between numerical and experimental results was found.

외란이 작용하는 비행선의 동적 반응 및 제어 (Dynamic Response and Control of Airship with Gust)

  • 우귀애;박인환;오세종;조겸래
    • 한국항공우주학회지
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    • 제30권6호
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    • pp.69-77
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    • 2002
  • 수직 돌풍이 작용하는 비행선의 비선형 방정식을 이용하여 종방향 운동에 대한 동적 반응을 살피고 제어기를 설계하였다. 비행선의 부가 질량과 부가 관성 모멘트는 동적 반응 및 정착시간을 지연시키므로 일반적인 항공기에 비해 매우 느리다. 본 논문에서는 사용된 비행선은 고도 500m에서 1,000m 상공을 순항하며 임무를 수행하기 위한 것으로, 그 고도에서 대기 조건은 바람이나 돌풍에 의해 영향을 받아 매우 불안정하다. 따라서 가상 질량 효과가 두드러지는 수직 평면에 작용하는 수직 돌풍이 비행선에 미치는 영향을 살펴보고, PID-제어기를 사용하여 제어기를 설계하였다. 돌풍이 작용하면 비행선은 평형 상태로 회복하지만, 회복 시간이 매우 오래 걸릴 뿐 아니라 속도에 있어 손실이 발생한다. 따라서 본 논문의 목적은 회복 시간은 빠르게 하는 것과 순항 속도로 되돌아가는 것이다. 제어기에 사용된 피라미터들은 안정 모드 해석으로부터 결정되었으며, 이때 제어 압력은 추력 및 엘리베이터 각이다.

비행 조건의 영향을 고려한 쿼드콥터형 무인비행체의 로터 공력 특성 예측 (Prediction for Rotor Aerodynamics of Quadcopter Type Unmanned Aerial Vehicle Considering Gust and Flight Conditions)

  • 박선후;은원종;신상준
    • 한국항공우주학회지
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    • 제46권10호
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    • pp.833-844
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    • 2018
  • 본 연구에서는 무인 회전익기의 종류인 쿼드콥터의 로터 블레이드에 대해 바람 및 비행 조건의 따른 공력특성을 예측하고자 한다. 돌풍 및 비행 조건들을 고려하기 위해 바람의 좌표계 변환 개념을 제시하였다. 강체 블레이드 플래핑 운동방정식을 고려한 깃 요소 및 운동량 이론을 이용해 개별 로터의 제자리, 전진, 상승 비행을 해석하였다. XFOIL을 사용하여 공력결과를 도출하였고, 개발된 BEMT를 이용하여 제자리 비행, 전진, 상승 조건의 검증을 수행했다. 또한 제자리 비행 실험 환경 구축 및 실험 결과와 개발된 BEMT의 비교 및 검증을 수행하였다.

난류-캐스케이드 상호작용 소음 예측을 위한 Perfectly Matched Layer 을 이용한 내부 입/출구 정상유동 경계조건의 개발 (Development of internal inflow/outflow steady mean flow boundary condition using Perfectly Matched Layer for the prediction of turbulence-cascade interaction noise)

  • 김대환;정철웅
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 춘계학술대회 논문집
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    • pp.521-526
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    • 2012
  • It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study(1) showed that Perfectly Matched Layer (PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

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난류-캐스케이드 상호작용 소음 예측을 위한 Perfectly Matched Layer을 이용한 내부 입/출구 정상유동 경계조건의 개발 (Development of Internal Inflow/outflow Steady Mean Flow Boundary Condition Using Perfectly Matched Layer for the Prediction of Turbulence-cascade Interaction Noise)

  • 김대환;정철웅
    • 한국소음진동공학회논문집
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    • 제22권7호
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    • pp.685-691
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    • 2012
  • It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study showed that perfectly matched layer(PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

한반도 영향 태풍의 월별 최대풍 특징과 사례 연구 - 태풍 루사·매미·곤파스·볼라벤을 대상으로 - (Characteristics of Monthly Maximum Wind Speed of Typhoons Affecting the Korean Peninsula - Typhoon RUSA, MAEMI, KOMPASU, and BOLAVEN -)

  • 나하나;정우식
    • 한국환경과학회지
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    • 제28권4호
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    • pp.441-454
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    • 2019
  • The present study analyzes the characteristics of 43 typhoons that affected the Korean Peninsula between 2002 and 2015. The analysis was based on 3-second gust measurements, which is the maximum wind speed relevant for typhoon disaster prevention, using a typhoon disaster prevention model. And the distribution and characteristics of the 3-second gusts of four typhoons, RUSA, MAEMI, KOMPASU, and BOLAVEN that caused great damage, were also analyzed. The analysis show that between May and October during which typhoons affected the Korean Peninsula, the month with the highest frequency was August(13 times), followed by July and September with 12 occurrences each. Furthermore, the 3-second gust was strongest at 21.2 m/s in September, followed by 19.6 m/s in August. These results show that the Korean Peninsula was most frequently affected by typhoons in August and September, and the 3-second gusts were also the strongest during these two months. Typhoons MAEMI and KOMPASU showed distribution of strong 3-second gusts in the right area of the typhoon path, whereas typhoons RUSA and BOLAVEN showed strong 3-second gusts over the entire Korean Peninsula. Moreover, 3-second gusts amount of the ratio of 0.7 % in case of RUSA, 0.8 % at MAEMI, 3.3 % at KOMPASU, and 21.8 % at BOLAVEN showed as "very strong", based on the typhoon intensity classification criteria of the Korea Meteorological Administration. Based on the results of this study, a database was built with the frequencies of the monthly typhoons and 3-second gust data for all typhoons that affected the Korean Peninsula, which could be used as the basic data for developing a typhoon disaster prevention system.

돌풍 대비용 직주 배치에 따른 계류안전성 민감도 분석 연구 (A Study on Analysis of Mooring Safety Sensitivity According to the Arrangement of Bitt Against Gust)

  • 김승연
    • 해양환경안전학회지
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    • 제26권7호
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    • pp.767-776
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    • 2020
  • 최근 지구온난화에 따른 기후변화에 따라 과거와는 다른 양상의 기상 변화가 발생하고 있으며, 해수 온도 상승으로 태풍의 대형화와 강도증가가 발생하고 있다. 이에 따라 선박이 접안 중 갑작스러운 돌풍 발생시 선박의 계류안전성 확보를 위해 사용할 수 있는 돌풍 대비용 직주의 필요성이 증대되고 있다. 본 연구에서는 항만 및 어항 설계기준상 곡주 및 직주 배치 기준을 분석하고 계류안전성 평가프로그램을 사용하여 12개 시나리오에 따른 직주 사용시 계류안전성 민감도 분석을 수행하였다. 평가 결과, 돌풍 대비용 직주에 선수 및 선미 브레스트라인을 추가하였을 경우, 일반적인 형태의 계류라인 배치에 비해 계류요소값이 감소하는 것으로 분석되었다. 본 연구 결과는 접안선박 및 항만의 특성을 고려한 돌풍 대비용 직주 배치를 제안하기 위한 기초 자료로 활용될 수 있으며, 부두에서 직주의 배치는 돌풍 발생시 선박운항자 측면에서 선박의 계류안전성을 확보하기 위한 효율적인 방안이 될 것으로 사료된다.