• 제목/요약/키워드: 격자-볼츠만 법

검색결과 55건 처리시간 0.02초

미소채널 내 회전교반기와 진동교반기에 의한 혼합향상의 연구 (A Study on Mixing Enhancement by Rotating and Oscillating Stirrers in the Micro Channel)

  • 김용대;맹주성;안상준
    • 대한기계학회논문집B
    • /
    • 제30권5호
    • /
    • pp.430-437
    • /
    • 2006
  • The mixing effect is studied by comparing rotating and oscillating stirrers in the micro channel. The cases of Re=10 to 80 with various stirring speeds are considered to analysis the effect of Re and stirrer speed for the mixing. Under Re=20, the oscillating stirrer represents better mixing rate than the rotating stirrer up to the critical stirrer speed which has a maximum efficiency. Over Re=30, the results of oscillating and rotating stirrer show that the faster the stirrer speed, the higher the mixing effect within the concerned stirrer speed range and the oscillating stirrer keeps the higher mixing rate. It was found that the mixing effect is a function which has an optimum of the Reynolds number and the stirrer speed. The D2Q9 Lattice Boltzmann Method is used due to the merits of calculation for the unsteady flow with moving boundary.

버티포트 이착륙을 고려한 지면 효과를 받는 UAM 항공기에 대한 공력소음 해석 연구 (Aeroacoustic Analysis of UAM Aircraft in Ground Effect for Take-off/Landing on Vertiport)

  • 양진용;이혁진;강민제;김은민;명노신;이학진
    • 항공우주시스템공학회지
    • /
    • 제17권2호
    • /
    • pp.26-37
    • /
    • 2023
  • 도시 교통 혼잡과 환경 문제에 대한 대안으로 차세대 비행체 Urban Air Mobility(UAM) 항공기 개발이 주목받고 있다. 이를 위해, UAM 항공기가 수직이착륙할 수 있는 플랫폼인 버티포트(Vertiport) 역시 논의되고 있다. 버티포트로 인한 지면 효과는 UAM 항공기의 공력과 소음 특성에 직접적인 영향을 미친다. UAM 항공기는 인구가 밀집된 도심에서 운용되므로 엄격한 소음 규제가 예상되므로, 설계단계에서 공기역학적 현상과 공력 소음의 정밀한 예측이 요구된다. 본 연구에서는 Lattice-Boltzmann Method(LBM) 시뮬레이션과 투과면 기반의 Ffowcs Williams and Hawkings(FW-H) 음향상사법을 이용하여 지면 효과에 대한 공력, 유동장, 원거리 소음 방사 특성을 분석하였다.

파수-주파수 분석을 이용한 자동차 옆 창문 표면 압력 섭동의 비압축성/압축성 성분 분해 (Decomposition of Surface Pressure Fluctuations on Vehicle Side Window into Incompressible/compressible Ones Using Wavenumber-frequency Analysis)

  • 이송준;정철웅
    • 한국소음진동공학회논문집
    • /
    • 제26권7호
    • /
    • pp.765-773
    • /
    • 2016
  • The vehicle interior noise caused by exterior fluid flow field is one of critical issues for product developers in a design stage. Especially, turbulence and vortex flow around A-pillar and side mirror affect vehicle interior noise through a side window. The reliable numerical prediction of the noise in a vehicle cabin due to exterior flow requires distinguishing between the aerodynamic (incompressible) and the acoustic (compressible) surface pressures as well as accurate computation of surface pressure due to this flow, since the transmission characteristics of incompressible and compressible pressure waves are quite different from each other. In this paper, effective signal processing technique is proposed to separate them. First, the exterior flow field is computed by applying computational aeroacoustics techniques based on the Lattice Boltzmann method. Then, the wavenumber-frequency analysis is performed for the time-space pressure signals in order to characterize pressure fluctuations on the surface of a vehicle side window. The wavenumber-frequency diagrams of the power spectral density shows clearly two distinct regions corresponding to the hydrodynamic and the acoustic components of the surface pressure fluctuations. Lastly, decomposition of surface pressure fluctuation into incompressible and compressible ones is successfully accomplished by taking the inverse Fourier transform on the wavenumber-frequency diagrams.

Lattice-Boltzmann Method를 이용한 이중구조팬의 공력소음 해석 및 저감 (Aeroacoustics Analysis and Noise Reduction of Dual Type Combined Fan using Lattice-Boltzmann Method)

  • 김우택;류민형;김진욱;호성환;조이상;조진수
    • 한국항공우주학회지
    • /
    • 제44권5호
    • /
    • pp.381-390
    • /
    • 2016
  • 본 연구에서는 이중구조팬의 소음특성을 알아보고 소음저감 방법으로 알려진 톱니형 뒷전(Serrated Trailing Egde)을 적용하여 이중구조팬의 소음을 저감시켰다. 해석에는 Lattice Boltzmann Method(LBM)를 이용한 비정상 전산해석을 수행하였으며 해석의 타당성을 평가하기 위하여 시험을 실시하였다. 이중구조팬은 일반적인 팬처럼 단일의 Blade Passing Frequency(BPF)를 갖는 것이 아니라 내부팬과 외부팬 각각의 BPF가 서로 다른 음역대에서 나타나는 것을 확인 하였다. 톱니형 뒷전을 내부팬에 적용하여 경계층에서의 구속와류와 뒷전에서의 와류흘림이 억제 또는 분산되고 광역소음뿐만 아니라 팬의 토크도 저감되었다.

사각 및 원형 팁의 횡운동에 의한 물 메니스커스 형상변화에 관한 연구 (Study on a Shape Deformation of Water Meniscus for the Rectangular and Circular Tips Moving Horizontally)

  • 김상선;손성완;하만영;윤현식;김형락
    • 설비공학논문집
    • /
    • 제23권12호
    • /
    • pp.843-851
    • /
    • 2011
  • A two-dimensional immiscible water meniscus deformation phenomena on a moving tip in a channel has been investigated by using lattice Boltzmann method involving two-phase model. We studied the behavior of a water meniscus between the tip and a solid surface. The contact angles of the tip and a solid surface considered are in the range from $10^{\circ}$ to $170^{\circ}$. The velocity of the tip used in the study are 0.01, 0.001, and 0.0001. The shapes of tip considered are rectangular and circular. The behavior of water confined between the tip and a solid surface depends on the contact angles of the tip and a solid surface, and the tip velocity. When the tip is moving, we can observe the various behaviors of shear deformation of a water meniscus. As time goes on, the behavior of a water meniscus can be classified into three different patterns which are separated from the tip or adhered to the tip or sticked to a solid surface according to the contact angles and the tip velocity.