• 제목/요약/키워드: Longitudinal acoustic Mode

검색결과 42건 처리시간 0.027초

Study of the unsteady pressure oscillations induced by rectangular cavities in a supersonic flow field

  • Krishnan L.;Ramakrishna M.;Rajan S.C.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2003년도 The Fifth Asian Computational Fluid Dynamics Conference
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    • pp.294-298
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    • 2003
  • The complex, unsteady, self-sustained pressure oscillations induced by supersonic flow past a rectangular cavity is investigated using numerical simulations. The present numerical study is performed using a parallel, multiblock solver for the two-dimensional, compressible Navier­Stokes equations. Open cavities with length-to-depth (L / D) ratio in the range 0.5 - 3.3 are considered. This paper sheds light on the cavity physics, cavity oscillatory mechanism, and the organisation of vortical structures inside the cavity. The vortex shedding phenomenon, the shear layer impingement event at the aft wall and the movement of the acoustic/compression wave within the cavity are well predicted. The vortical structures· and the source of the acoustic disturbances are found to be located near the aft wall of the cavity. With the increase in the cavity length, strong recompression of the flow near the aft wall leading to a sudden jump in the cavity form drag is observed. The estimated cavity tones are in good agreement with the available semi­empirical relation. Multiple peaks are noticed in deep and long cavities. For the present free­stream Mach number 1.71, it is observed that around L/D=2.0, the cavity oscillatory mechanism changes from the transverse to longitudinal oscillatory mode. The effects of this transition on various fluid dynamics and acoustic properties are also discussed.

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환형노즐을 모사한 캔 연소기에서 Symmetry Breaking에 의한 종-방향 연소불안정성 제어 연구 (Control of the Longitudinal Instability by Symmetry Breaking in the Can Burner Simulating Annular Nozzle)

  • 이희도;김재현;이기만
    • 한국추진공학회지
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    • 제25권2호
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    • pp.66-78
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    • 2021
  • 본 연구에서는 환형연소기에서 연소불안정성이 발생하는 당량비 조건과 노즐 개수에 따라서 대칭성파괴(Symmetry Breaking) 효과를 비교하였다. 일반적으로 환형연소기에서는 연소실의 길이가 짧으므로 종-방향 연소불안정성이 잘 발생하지 않으나, 발전용 가스터빈시스템의 트랜지션피스(Transition piece) 같은 덕트가 존재하였을 때는 연소불안정성이 발생하였다. 이 경우 덕트로 인하여 종-방향의 불안정성 모드만 관찰되었다. 5개의 희박노즐 개수와 당량비 조건에 따라서 대칭성파괴 특성을 조사하였는데, 당량비가 감소할수록 대칭성파괴 효과가 빠르게 발생하여 불안정성이 극적으로 사라지면서 진폭이 크게 감소하였다. 또한, 희박노즐 개수가 증가할수록 당량비 감소와 같은 현상이 나타나는 것을 확인하였다.

PIC simulation study of the turbulence of the Alfven ion-cyclotron waves induced by electromagnetic ion-cyclotron instability

  • Kaang, Helen H.;Ryu, Chang-Mo;Mok, Chinook;Rha, Ki-Cheol
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2011년도 한국우주과학회보 제20권1호
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    • pp.29.3-29.3
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    • 2011
  • The turbulence in the nonlinear regime of the electromagnetic ion-cyclotron (EMIC) instability are investigated via a particle-in-cell (PIC) simulation. EMIC instability arises from anisotropic ion temperature and excites the Alfven ion-cyclotron (AIC) waves. The excited AIC waves undergo inverse-cascade via the nonlinear wave interaction of two AIC and one ion density modes. Induced ion density modes are the normal and second harmonic ion-acoustic (IA) waves. They have the same group velocity, but the second harmonic IA mode only generates the longitudinal electric field.

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연료-공기 비혼합도가 희박예혼합 연소 특성에 미치는 영향 (Effects of Fuel-Air Unmixedness on Lean Premixed Combustion Characteristics)

  • 김대현;이종호;전충환;장영준
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제24회 KOSCO SYMPOSIUM 논문집
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    • pp.133-139
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    • 2002
  • The lean premixed technique has been proven very efficient in reducing NOx emissions from gas turbine combustors. However combustion instability is susceptible to occur in lean premixed combustor. So laboratory-scale dump combustor was used to understanding the underlying mechanisms causing combustion instabilities. In this study, tests were conducted at atmospheric pressure and inlet air was up to $360^{\circ}C$ with natural gas. The observed instability was a longitudinal mode with a frequency of ${\sim}341.8Hz$. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various equivalence ratio. Combustion instability was observed to occur at higher value of equivalence ratio(>0.69). This study was performed to investigate the effects of equivalence ratio and fuel split measuring NOx and acoustic wave. The results reveal the effect of fuel-air unmixedness on lean premixed combustor.

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Silo 형 가스터빈 연소기에서 발생하는 연소진동 분석 및 저감 (Analysis of Combustion Oscillation and its Suppression in a Silo Type Gas Turbine Combustor)

  • 서석빈;안달홍;차동진;박종호
    • 설비공학논문집
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    • 제21권2호
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    • pp.126-130
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    • 2009
  • The present study describes an investigation into the characteristics of combustion oscillation and its suppression instability of a silo type gas turbine combustor in commercial power plant. Combustion oscillation is occurred the combustor in near full load during operation. As a result of FFT analysis of the combustion dynamics, the frequency of the oscillation is analyzed as the 1'st longitudinal mode of acoustic resonance of the combustor. For suppress of the instability, combustion tuning with adjust of fuel valve schedule is carried out, which changes equivalent ratio of each burners. As the result, the oscillation is successfully reduced with meeting the level of NOx emission regulation.

GE 7FA+e DLN-2.6 연소기를 모사한 모형 가스터빈 연소기의 연소불안정 특성에 대한 실험적 연구 (An Experimental Investigation of Combustion Characteristics in a Model Combustor by Reproduction of GE 7FA+e DLN-2.6 Gas Turbine)

  • 김민기;이장수;박성순;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.231-235
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    • 2009
  • 본 연구의 목적은 실제로 서인천 발전본부에서 운용하고 있는 GE 7FA+e DLN 2.6 가스터빈 연소기의 연소특성과 배기배출물에 대한 제어 연구를 소개하고 모형 가스터빈 연소기의 연소동특성 및 연소불안정 현상을 확인하고자 한다. 모형 연료노즐은 실제의 1/3 크기로 상사하여 제작되었고, 실제 노즐과 동일한 각도의 2단 스월러(swirl vane)를 가지고 있다. Plenum과 연소기의 형상은 실 가스터빈과 유사한 음향학적 특성을 가질 수 있도록 설계되었고 실험은 공기온도, 노즐출구 속도, 당량비, 연소실 길이를 변수로 이루어졌으며, 그 결과 연소실의 연소불안정 mode는 각각의 실험 변수에 따라서 연소실의 공진주파수의 영향, 연소온도와 공기-연료 혼합기 분포에 의해서 mode가 전이되는 현상을 확인하였다.

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Development of a Guided Wave Technique for the Inspection of a Feeder Pipe in a Pressurized Heavy Water Reactor

  • Cheong, Yong-Moo;Lee, Dong-Hoon;Kim, Sang-Soo;Jung, Hyun-Kyu
    • Corrosion Science and Technology
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    • 제4권3호
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    • pp.108-113
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    • 2005
  • One of the recent safety issues in the pressurized heavy water reactor (PHWR) is the cracking of the feeder pipe. Because of the limited accessibility to the cracked region and a high dose of radiation exposure, it is difficult to inspect all the pipes with the conventional ultrasonic method. In order to solve this problem, a long-range guided wave technique has been developed. A computer program to calculate the dispersion curves in the pipe was developed and the dispersion curves for the feeder pipes in PHWR plants were determined. Several longitudinal and/or flexural modes were selected from the review of the dispersion curves and an actual experiment has been carried out with the specific alignment of the piezoelectric ultrasonic transducers. They were confirmed as L(0,1)) and/or flexural modes(F(m,2)) by the short time Fourier transformation(STFT) and were sensitive to the circumferential cracks, but not to the axial cracks in the pipe. An electromagnetic acoustic transducers(EMAT) was designed and fabricated for the generation and reception of the torsional guided wave. The axial cracks were detected by a torsional mode(T(0,1)) generated by the EMAT.

연료 과농 가스발생기의 연소 안정성 특성 연구 (Combustion Stability Characteristics of Fuel-Rich Gas Generators)

  • 서성현;한영민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.119-122
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    • 2007
  • 본 연구에서는 가스발생기의 연소 안정 특성을 파악하기 위해 실험적 방법을 적용하였다. 액체산소와 Jet A-1을 추진제로 사용하며 연료 과농 상태에서 작동하는 실험 가스발생기는 연소실 축 방향 공진 모드에 결합된 1200 Hz 대역의 고주파 연소불안정을 겪었다. 이 연소불안정의 발생 유무는 연소실 출구부의 음향 경계 조건과 화염의 열 발생 축 방향 위치에 매우 민감하게 반응하였다. 결과적으로 단일 분사기 노즐 크기 증가에 의한 화염의 축 방향 길이 증가는 연소안정성을 확연하게 향상시켰다.

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음향광변조기를 이용한 고분해능의 헤테로다인 간섭식 열팽창 측정기술 (High resolution heterodyne interferometric technique with AOM for measuring the thermal expansion)

  • 최병일;이상현;김종철;임동건
    • 한국광학회지
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    • 제13권6호
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    • pp.530-536
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    • 2002
  • 열팽창계수의 정확한 측정은 재료과학이나 공업기술 분야에서 가장 중요한 요구량 중의 하나이다. 음향광변조기(AOM)를 이용한 고분해능 간섭식 열팽창계를 제작하여 성능검사를 하였다. 이 계는 이중광로 헤테로다인 간섭계와 복사열 전기로로 구성되어, 정밀한 변위의 측정과 시료의 신속한 가열 및 냉각이 가능토록 하였다. 또한 레이저의 주파수 안정화를 위하여 2차 맥놀이 주파수를 이용한 3종모드 안정화 He-Ne 레이저를 제작하였으며, 이때의 주파수 안정도는 5$\times$$10^{-9}$이었다. 제작된 계의 길이 측정은 실온에서 1100k온도영역에서 나노미터 정도의 정밀도를 주었다.

Reflection and propagation of plane waves at free surfaces of a rotating micropolar fibre-reinforced medium with voids

  • Anya, Augustine Igwebuike;Khan, Aftab
    • Geomechanics and Engineering
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    • 제18권6호
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    • pp.605-614
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    • 2019
  • The present paper seeks to investigate propagation and reflection of waves at free surfaces of homogeneous, anisotropic and rotating micropolar fibre-reinforced medium with voids. It has been observed that, in particular when P-wave is incident on the free surface, there exist four coupled reflected plane waves traveling in the medium; quasi-longitudinal displacement (qLD) wave, quasi-transverse displacement (qTD) wave, quasi-transverse microrotational wave and a wave due to voids. Normal mode Analysis usually called harmonic solution method is adopted in concomitant with Snell's laws and appropriate boundary conditions in determination of solution to the micropolar fibre reinforced modelled problem. Amplitude ratios which correspond to reflected waves in vertical and horizontal components are presented analytically. Also, the Reflection Coefficients are presented using numerical simulated results in graphical form for a particular chosen material by the help of Mathematica software. We observed that the micropolar fibre-reinforced, voids and rotational parameters have various degrees of effects to the modulation, propagation and reflection of waves in the medium. The study would have impact to micropolar fibre-reinforecd rotational-acoustic machination fields and future works about behavior of seismic waves.