• 물과 미래
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• 제29권5호
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• pp.139-150
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• 1996

본 논문에서는 수리학적 유역추적 모형인 선형 Muskingum-Cunge(M-C)법에 있어서 격자간격과 같은 수치적 인자의 변화가 단위폭사면에서의 유출수문곡선에 미치는 영향을 소개한다. 수치계산의 결과에 의하면, 유출특성은 수치적 또는 물리적으로 의미를 갖는 Courant 수 C 및 cell Reynolds 수 D의 값에 좌우되는데, C 값은 1에 접근할수록 D 값은 증가할수록 수치분산에 의한 진동은 발생하기 어렵다. C<1인 경우는 수치진동이 이동파의 전방에 발생한다. C>1인 경우는 파의 후방에 발생하는데, 이 때는 수치확산의 효과로 인해 수치진동은 작아지거나 사라진다. 특성구간길이 L의 값이 작은 사면(예, 급경사사면)의 경우, M-C법은 kinematic 법과 마찬가지로 파의 감쇠를 보이지 않는다. 한편 L의 값이 큰 사면(예, 완경사 사면)에서는 M-C법은 큰 거리격자간격 (Δx)에서도 큰 D(= L/ΔX)의 값을 갖게 되어 C에 거의 관계없이 diffusion wave를 잘 재현한다. 따라서 완경사 유역의 추적에 있어 M-C 법의 적용은 매우 유효하리라고 생각된다.

• Journal of Mechanical Science and Technology
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• 제15권5호
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• pp.646-655
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• 2001

This paper reports the effects of nozzle exit boundary layer swirl on the instability modes of underexpanded supersonic jets emerging from plane rectangular nozzles. The effects of boundary layer swirl at the nozzle exit on thrust and mixing of supersonic rectangular jets are also considered. The previous study was performed with a 30°boundary layer swirl (S=0.41) in a plane rectangular nozzle exit. At this study, a 45°boundary layer swirl (S=1.0) is applied in a plane rectangular nozzle exit. A three-dimensional unsteady compressible Reynolds-Averaged Navier-Stokes code with Baldwin-Lomax and Chiens $\kappa$-$\xi$ two-equation turbulence models was used for numerical simulation. A shock adaptive grid system was applied to enhance shock resolution. The nozzle aspect ratio used in this study was 5.0, and the fully-expanded jet Mach number was 1.526. The \"flapping\" and \"pumping\" oscillations were observed in the jets small dimension at frequencies of about 3,900Hz and 7,800Hz, respectively. In the jets large dimension, \"spanwise\" oscillations at the same frequency as the small dimensions \"flapping\" oscillations were captured. As reported before with a 30°nozzle exit boundary layer swirl, the induction of 45°swirl to the nozzle exit boundary layer also strongly enhances jet mixing with the reduction of thrust by 10%.

• Journal of Magnetics
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• 제20권4호
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• pp.460-465
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• 2015

The paper presents methodologies and results concerning one- and two-dimensional numerical modeling of radio frequency oscillations in a coaxial transmission line fed with a short pulse of electric current. The line is partially filled with a ferrite material, magnetized longitudinally close to saturation. The 2D model has permitted analyzing, for the first time in the art, the spatial structure and dynamics of the wave field within the radially non-uniform cross-section planes of the non-linear and dispersive guiding structure. This opens ways for optimizing size parameters of the line and the extent to which it is filled with the ferromagnetic material, thus increasing the line's electric strength and intensity of the r.f. oscillations.

• 한국초전도ㆍ저온공학회논문지
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• 제23권1호
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• pp.1-6
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• 2021

Thermoacoustic oscillations (TAOs) could be often observed in liquid helium cryogenic system especially in half-open tubes. These tubes have closed warm end (300K) and open cold end (usually 4.4K). This phenomenon significantly induces additional heat load to cryogenic system and other undesirable effects. This work focuses on using computational fluid dynamics (CFD) method to study TAOs in liquid helium. The calculated physical model, numerical scheme and algorithm, and wall boundary conditions were introduced. The simulation results of onset process of thermoacoustic oscillations were presented and analyzed. In addition, other important characteristics including phase relation and frequency were studied. Moreover, comparisons between experiments and the CFD simulations were made, which demonstrated thevalidity of CFD simulation. CFD simulation can give us a better understanding of onset mechanism of TAOs and nonlinear characteristics in liquid helium cryogenic system.

• Advances in aircraft and spacecraft science
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• 제9권5호
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• pp.479-491
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• 2022

This work concerns the investigation of a Q1D methodology employed to study pressure oscillations in solid rocket motors driven by hydrodynamic instabilities. A laboratory-scale solid motor designed to develop vortex-shedding phenomena is analyzed for the whole firing time. The comparison between numerical results and experimental data shows good agreement regarding pressure oscillations signature, especially in the flute-mode behavior, the typical oscillations frequency trend present in any motor liable to hydrodynamic instabilities. Such result ensures the model capability to cope with this particular kind of pressure oscillations source, allowing the investigation of the phenomenon with a lighter and cost savings methodology than CFD simulations.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 춘계학술대회 논문집
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• pp.119-122
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• 2009

본 연구에서는 2차원 초음속 공동유동에서 발생하는 압력진동을 제어하기 위하여 수치해석적 연구를 수행하였다. 본 계산에서는 압력진동을 제어하기 위하여 보조공동의 형상을 변화시켰으며, 유동의 마하 수를 1.50, 1.83 그리고 2.50로 변화시켰다. 그 결과, 보조공동은 압력진동을 상당히 감소시켰으며, 압력진동의 제어효과는 유동의 마하수와 보조공동의 상세형상에 크게 의존함을 알았다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 12th Asian Congress of Fluid Mechanics
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• pp.53.2-53.2
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• 2008

• 천문학회지
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• 제34권4호
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• pp.265-269
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• 2001

We present preliminary numerical simulations of tilted-disk accretion around a rotating black hole. Our goal is to explore whether hydrodynamic instabilities near the Bardeen-Petterson radius could be responsible for generating moderate-frequency quasi-periodic oscillations in X-ray binaries. We review the relevant general relativistic hydrodynamic equations, and discuss preliminary results on the structure and dynamics of a thin, Keplerian disk.

• 대한기계학회논문집B
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• 제31권2호
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• pp.141-150
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• 2007

This paper presents a lumped model to predict crosstalk characteristics of thermally driven inkjet print heads. Using the lumped R-C model, heating characteristics of the head are predicted to be in agreement with IR temperature measurements. The inter-channel crosstalk is simulated using the lumped R-L network. The values of viscous flow resistance, R and flow inertance, L of connecting channels are adjusted to accord with the 3-D numerical simulation results of three adjacent jets. The crosstalk behaviors of a back shooter head as well as a top shooter head have been investigated. Predictions of the proposed lumped model on the meniscus oscillations are consistent with numerical simulation results. Comparison of the lumped model with experimental results identifies that abnormal two-drop ejection phenomena are related to the increased meniscus oscillations because of the more severe crosstalk effects at higher printing speeds. The degree of crosstalk has been quantified using cross-correlations between neighboring channels and a critical channel dimension for acceptable crosstalk has been proposed and validated with the numerical simulations. Our model can be used as a design tool for a better design of thermal inkjet print heads to minimize crosstalk effects.

• 한국추진공학회지
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• 제6권2호
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• pp.75-84
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• 2002

고체 추진 로켓 내부 연소실의 비정상 유동을 수치적으로 해석하였다. 완전 보존식을 이용하여 2 차원 축-대칭 연소실 안의 연소 불안정을 해석하기 위한 수치 기법을 구성하였는데 비정상 유동을 해석하기 위한 수정된 $\kappa$-$\varepsilon$ 난류 모델이 사용되었다. 이산화한 지배 방정식은 연관된 경계 조건을 포함하여 dual time-stepping 방법으로 시적분 하였다. 정상 상태의 계산을 기반으로 연소실 내의 천이 압력파의 비정상 상태를 수치적으로 모사하기 위하여 압력 펄스 및 압력 변동을 연소실 상단에 부과하였다. 로켓 모터 연소실 내의 다양한 정상 상태 및 비정상 상태의 특성을 계산 및 해석하였다.