• 제목/요약/키워드: Aero-acoustic Noise

검색결과 48건 처리시간 0.023초

생체모방공학을 적용한 고속철 차간 공간의 공력소음 연구 (Analysis of aerodynamic noise at inter-coach space of high speed trains based on biomimetic analogy)

  • 한재현;김태민;김정수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2011년도 추계학술대회 논문집
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    • pp.711-716
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    • 2011
  • Today, high-speed trains enjoy wide acceptance as fast, convenient and environment-friendly means of transportation. However, increase in the speed of the train entails a concomitant increase in the aerodynamic noise, adversely affecting the passenger comfort. At the train speed exceeding 300 km/h, the effects of turbulent flows and vortex sheddding are greatly amplified, contributing to a significant increase in the aerodynamic noise. Drawing a biomimetic analogy from low-noise flight of owl, a method to reduce aerodynamic noise at inter-coach space of high-speed trains is investigated. The proposed method attempts to achieve the noise reduction by modifying the turbulent flow and vortex shedding characteristics at the inter-coach space. To determine the aerodynamic noise at various train speeds, wind tunnel testing and numerical CFD (Computational Fluid Dynamics) simulation for the basic inter-coach spacing model are carried out, and their results compared. The simulation and experimental results reveal that there are discrete frequency components associated with turbulent air flow at constant intervals in the frequency domain

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복합 CAA 방법과 FRPM 기법을 이용한 냉장고 얼음제조용 원심팬의 광대역 소음 예측 (Broadband Noise Prediction of the Ice-maker Centrifugal Fan in a Refrigerator Using Hybrid CAA Method and FRPM Technique)

  • 허승;김대환;정철웅
    • 한국음향학회지
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    • 제31권6호
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    • pp.391-398
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    • 2012
  • 본 연구에서는 기존의 RANS(Reynolds Averaged Navier Stokes) 방정식을 이용하는 복합 CAA(Computational AeroAcoustics) 방법에 광대역 소음원 생성을 위한 FRPM(Fast Random Particle Mesh) 기법을 적용하여 원심팬 광대역 소음 예측을 수행하였다. 먼저, RANS 방정식을 이용하여 원심팬 주위의 유동장을 예측하여 주요한 소음원 영역을 추론하고, 추론된 소음원 영역에 FRPM 기법을 적용하여 통계적 특성을 만족하는 난류를 재생하였다. RANS 방정식으로부터 해석된 유동장과 FRPM 기법으로부터 재생된 유동장을 이용하여 합성한 유동장에 음향상사법(Acoustic Analogy)을 적용하여 원심팬의 소음원을 생성하였다. 생성된 원심팬의 소음원을 경계요소법(Boundary Element Method)으로 구현된 선형전파모델에 적용하여 원심팬의 광대역 소음을 예측하였다. 원심팬에 대한 소음 측정값과의 비교를 통하여 제안된 기법이 원심팬의 순음 소음 및 광대역 소음 예측에 효과적임을 확인하였다.

복합형 수직축 풍력발전기의 유동소음특성에 관한 수치적 고찰 (Numerical Investigation on the Flow Noise Characteristics of the Hybrid Vertical-axis Wind Turbine)

  • 김상현;정철웅
    • 한국음향학회지
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    • 제33권6호
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    • pp.351-357
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    • 2014
  • 본 논문에서는 복합형 수직축 풍력발전기의 유동소음특성에 관한 연구를 수행하였다. 복합형 수직축 풍력발전기는 Savonius형과 Darrieus형을 동시에 사용하여 두 풍력발전기의 장점을 극대화하여 단점을 상쇄시키는 새로운 개념의 수직축 풍력발전기이다. 본 연구에서는 이러한 특성을 갖는 복합형 수직축 풍력발전기에 대하여, 복합 전산공력음향학 기법을 이용하여 풍력발전기에서 발생하는 유동소음을 예측하였다. 먼저, 전산유체역학 기법을 이용하여 터빈 주위의 비정상유동장을 예측하였다. 다음으로, 예측한 비정상유동장에 음향상사법을 적용하여 터빈으로부터 방사하는 유동소음을 예측하였다. 해석결과를 바탕으로 복합형 수직축 풍력발전기의 유동소음특성을 분석하였고, 이를 Savonius형 및 Darrieus형의 유동소음특성과 비교하였다.

STAR-CCM+를 이용한 썬루프 버페팅 유동 소음 해석 (Numerical Analysis of Sunroof Buffeting using STAR-CCM+)

  • 사티쉬 본투;프레드 멘돈카;김귀연;백영렬
    • 한국소음진동공학회논문집
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    • 제24권3호
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    • pp.213-218
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    • 2014
  • 썬루프 버페팅 소음의 고유특성을 의미하는 속도에 따른 소음강도의 증-감쇠 현상을 살펴보고자, HSM(Hyundai simplified model) 형상에 대해서 유동소음 해석 프로그램인 STAR-CCM+을 통하여 전체 차속 범위에 걸쳐 시험과 비교 검토하였다. 차량 내부의 재질에 따른 압축성 효과 및 감쇠효과는 인공 압축성과 감쇠 보정 기법인 FRET(frequency response test)를 이용하였다. 시뮬레이션 결과는 특정 속도에서 나타나는 소음 강도의 증-감쇠 시험결과를 매우 잘 예측하였으며 최대 SPL 수치도 정확히 예측하였다. 이는 썬루프 개방에 의해 발생하는 전단면에서의 유동 박리 주파수를 유동 소음 해석인 STAR-CCM+가 전 차속에 걸쳐서 매우 잘 예측하고 있음을 나타낸다.

Computation of Turbulent Flows and Radiated Sound From Axial Compressor Cascade

  • Lee, Seungbae;Kim, Hooi-Joong;Kim, Jin-Hwa;Song, Seung-Jin
    • Journal of Mechanical Science and Technology
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    • 제18권2호
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    • pp.272-285
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    • 2004
  • The losses at off-design points from a compressor cascade occur due to the deviation from a design incidence angle at the inlet of the cascade. The self-noise from the blade cascade at off-design points comes from a separated boundary layer and vortex sheddings. If the incidence angle to the cascade increases, stalling in blades may occur and the noise level increases significantly. This study applied Large-Eddy Simulations (LES) using deductive and deductive dynamic SGS models to low Mach-number, turbulent flow with each incidence angle to the cascade ranging from -40$^{\circ}$ to +20$^{\circ}$ and compared numerical predictions with measured data. It was observed that the oscillating separation bubbles attached to the suction surface do not modify wake flows dynamically for cases of negative incidence angles. However, an incidence angle greater than 8$^{\circ}$ caused a separated vortex near the leading edge to be shed downstream and created stalling. The computed performance parameters such as drag coefficient and total pressure loss coefficient showed good agreement with experimental results. Noise from the cascade of the compressor is summarized as sound generated by a structure interacting with unsteady, turbulent flows. The hybrid method using acoustic analogy was observed to closely predict the measured overall sound powers and directivity patterns at design and off-design points of blade cascade.

팬헤드의 단순 형상 모델을 이용한 판토그라프 공력소음 발생 특성 분석 및 저감 방안 (Analysis of Aerodynamic Noise Generation from Pantograph Using Panhead Models of Simple-Geometry and Its Reduction)

  • 이석근;양원석;고효인;박준홍
    • 한국철도학회논문집
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    • 제15권6호
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    • pp.531-536
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    • 2012
  • 판토그라프 팬헤드의 공력소음 발생의 주요 인자와 영향을 미치는 변수를 분석하였다. 팬헤드 주변의 유체 유동과 결과적인 소음 방사를 분석하기 위해, 수치해석적인 방법 중 하나인 격자볼츠만 방법으로 팬헤드 단순모델을 사용했다. 풍동실험을 통해 측정된 결과로 시뮬레이션 결과를 검증했다. 와흘림이 주요한 공력소음 발생원인이며 Strouhal수, 유체의 속도 및 판토그라프의 형상에 영향을 받았다. 이 논문에 사용된 직사각형 형상을 통해 양력의 발생을 증가시키면서 방사 소음을 줄이는 팬헤드의 설계가 가능함을 제시하였다. 또한 통로나 유선 형상을 이용해 와흘림을 최소로 줄이면, 방사 소음을 크게 저감하는 형상의 설계가 가능함을 구축된 해석모델을 이용하여 검증하였다.

저소음 청소기 개발 (Low Noise Vacuum Cleaner Design)

  • 주재만;이준화;홍승기;오장근;송화규
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 추계학술대회논문집
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    • pp.939-942
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    • 2007
  • Vacuum cleaner is a close life product that can remove various dusts from our surroundings. However well vacuum cleaner clean our environments, many people are looking away from it, due to its loud noise. Its noise causes a big trouble in the usual life, for example, catch calls, TV watching and discussing etc. To reduce these inconveniences, noise reduction methods and systematic design of low noise vacuum cleaner are studied in this paper. At first, sound quality investigation is performed to get the noise level and quality that make people TV watching and catch calls available. Based on the European and domestic customer SQ survey result, sound power, peak noise level and target sound spectrum guideline are studied and introduced. As a second, precise product sound spectrums are designed into each part based on the sound quality result. Fan-motor, brush, mainbody, cyclone spectrums are decided to get the final target sound based on the contribution level. Fan-motor is the major noise source of vacuum cleaner. Specially, its peak sound, RPM peak and BPF Peak, cause the people nervous. To reduce these peak sounds, high rotating impeller and diffuser are focused due to its interaction. A lot of experimental and numerical tests, operation points are investigated and optimization of flow path area between diffusers is performed. As a bagless device, cyclones are one of the major noise sources of vacuum cleaner. To reduce its noise, previous research is used and adopted well. Brush is the most difficult part to reduce noise. Its noise sources are all comes from aero-acoustic phenomena. Numerical analysis helps the understanding of flow structure and pattern, and a lot of experimental test are performed to reduce the noise. Gaps between the carpet and brush are optimized and flow paths are re-designed to lower the noise. Reduction is performed with keeping the cleaning efficiency and handling power together and much reduction of noise is acquired. With all above parts, main-body design is studied. To do a systematic design, configuration design developments technique is introduced from airplane design and evolved with each component design. As a first configuration, fan-motor installation position is investigated and 10 configuration ideas are developed and tested. As a second step, reduced size and compressed configuration candidates are tested and evaluated by a lot of major factor. Noise, power, mass production availability, size, flow path are evaluated together. If noise reduction configuration results in other performance degrade, the noise reduction configuration is ineffective. As a third configuration, cyclones are introduced and the size is reduced one more time and fourth, fifth, sixth, seventh configuration are evolved with size and design image with noise and other performance indexes. Finally we can get a overall much noise level reduction configuration. All above investigations are adopted into vacuum cleaner design and final customer satisfaction tests in Europe are performed. 1st grade sound quality and lowest noise level of bagless vacuum cleaner are achieved.

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커버 형상을 고려한 고속전철 팬터그래프 공력특성의 수치해석적 연구 (INVESTIGATION FOR THE AERODYNAMIC CHARACTERISTICS OF HIGH SPEED TRAIN PANTOGRAPH WITH COVER)

  • 강형민;김철완;조태환;김동하;윤수환;권혁빈
    • 한국전산유체공학회지
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    • 제17권3호
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    • pp.18-24
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    • 2012
  • The aerodynamic performance of the pantograph on a high speed train was compared for different pantograph covers which are designed to block the aero-acoustic noise from the pantograph. For the study, two types of cover are designed: wedge and cone types. The lift force of pantograph with cover was compared with the force of pantograph only. The comparison clarified that the cone type cover increases the sideslip angle of the flow and decreases the lift force considerably. However, the wedge type cover changes the flow direction upward and increases the lift force of the pan head. This increment of lift force compensates the decrement of lift force caused by the blocking of the flow into the pantograph lower frame due to cover. Therefore, in case of the wedge type cover, the overall lift force changes slightly compared with the cone type cover.