• 한국전산유체공학회지
• /
• 제10권4호통권31호
• /
• pp.32-38
• /
• 2005

Present study simulates oscillatory supersonic impinging jet flows using the axisymmetric Navier-Stokes code. To capture the salient features of flow oscillation and overcome the divergence during the initial transient period, several tests have been conducted for the grid and time step sizes. The results also show that the effects of the inlet flow condition at the nozzle exit and turbulence on the oscillatory behavior of supersonic impinging jets are negligible. Frequencies of the surface pressure oscillation obtained by the selected numerical method are in good accord with the measured impinging tones for various cases of nozzle-to-plate distance. Two seemingly different staging behaviors with nozzle-to-plate distance and nozzle pressure variations are found to correlate well if the frequency and distance are normalized by the length of the first shock cell.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2004년도 춘계 학술대회논문집
• /
• pp.154-159
• /
• 2004

Numerical simulations of supersonic impinging jet flows are carried out using the axisymmetric Navier-Stokes code. This paper focuses on the oscillatory flow features associated with the variation of the nozzle pressure ratio and nozzle-to-plate distance. Frequencies of the surface pressure oscillation from computational results are in accord with the measured impinging tones for various cases of nozzle-to-plate distance. The variation of this frequency with distance show a staging behavior. Computed results for the case of nozzle pressure ratio variation for a fixed nozzle-to-plate distance also demonstrate a staging behavior. These two seemingly different staging behaviors are found to obey the same frequency-distance characteristics when the frequency and the distance are normalized by using the length of the shock cell.

• 한국안전학회지
• /
• 제32권2호
• /
• pp.112-116
• /
• 2017

Present study investigated the influence of time step size, turbulent eddy viscosity, and the number of layer on rapid and unsteady propagation of dam break flow. When the time step size had a value such that it resulted in Cr of 0.89, a significant numerical oscillation was observed in the vicinity of the wave front. Higher turbulent viscosity ensured smooth and mild slope of velocity and water stage compared with the flow behavior by no viscosity. The vertical velocity at the lower layer positioned near the bottom showed lower velocity compared with other layers.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
• /
• pp.295-298
• /
• 2007

본 연구에서는 초음속 공동유동장에서 발생하는 압력변동을 저감하기 위한 피동제어방법의 유용성을 실험 및 수치해석적으로 조사하였다. 피동제어방법으로 사각 공동내 상류 벽면에 sub-cavity를 설치하였다. 공동내 하류벽면에 센서를 설치하여 압력변동 값을 실험적으로 측정하였으며, 측정된 압력변동값을 FFT변환하여 주파수 분석을 하였다. 수치계적으로는 공동내 압력변동 특성을 살펴보기 위해 3차원 비정상 Navier-Stokes 방정식에 유한체적법을 적용하여 유동장을 모사하였으며, 유동의 난류상태량들은 LES 방법을 사용하여 계산하였다. 본 연구에서 얻어진 결과는 다음과 같다. 공동유동에서 진동 특성은 공동 하류벽면에서 발생하는 압력진동에 의존한다. 특히 leading tip 두께와 sub-cavity 크기가 진동 저감효과에 주요 인자이다.

• 전기전자학회논문지
• /
• 제24권1호
• /
• pp.132-139
• /
• 2020

공기청정기에 사용되는 이오나이저 모듈은 권선형 transformer를 사용하여 방전전극인 HV+/HV-에 3.5KV/-4KV의 고전압을 공급하여 carbon fiber brush의 전계 방사에 의해 양이온과 음이온을 발생시킨다. 기존의 MCU를 이용한 이오나이저 모듈 회로는 PCB 사이즈가 크고 가격이 비싼 단점이 있고, 기존의 ring oscillator를 이용한 게이트 구동 칩은 oscillation 주기가 PVT(Process-Voltage-Temperature) 변동에 민감하고 HV+와 GND, HV-와 GND의 단락에 의한 fault detection 기능이 없으므로 화재나 감전의 위험이 있다. 그래서 본 논문에서는 7bit binary UP counter를 이용하여 PVT 변동이 있더라도 oscillation 주기를 조절하여 HV+ 전압이 목표 전압에 도달하게 한다. 그리고 HV+와 GND 사이의 단락을 검출하기 위한 HV+ short fault detection 회로, HV-와 GND 사이의 단락을 검출하기 위한 HV- short fault detection 회로와 HV+가 과전압 이상으로 올라가는 것을 검출하기 위한 OVP(Over-Voltage Protection) 회로를 새롭게 제안하였다.

• 미생물학회지
• /
• 제24권3호
• /
• pp.270-275
• /
• 1986

Pseudomonas carboxydovorans와 Acinetobacter sp.l에 존재하는 일산화탄소 산화효소의 세포내 분포양상을 조사 하기 위 하여 엘 산 화탄소를 이 용하여 성장한 세균을 초음파로 파괴하거나 세균의 spheroplast을 만들어 삼투 충격으로 파괴한 후 soluble fraction과 particulate fraction에서의 일산화탄소 산화효소의 환성분포를 조사허여 비교하였다. 세균을 초음파로 파괴하였을 때는 crude cell extract에 존재하면 효소환성의 대부분이 soluble fracttion에서 검출되었다. 그러나 sphe roplas를 삼투충격으로 파괴하였을 때는 효소활성 이 세포막부분에서만 나타났다. 이와 같은 결과는 이 세균들의 일산화탄소 산화효소가 세포막에 느슨하게 붙이 있음을 시사하고 있다.

• Journal of Mechanical Science and Technology
• /
• 제16권11호
• /
• pp.1448-1456
• /
• 2002

The present study addresses the flow characteristics involved in the self-induced oscillations of the underexpanded jet impinging upon a cylindrical body. Both experiment and computational analysis are carried out to elucidate the shock motions of the self-induced oscillations and to find the associated major flow factors. The underexpanded sonic jet is made from a nozzle and a cylindrical body is placed downstream to simulate the impinging jet upon an obstacle. The computational analysis using TVD scheme is applied to solve the axisymmetric, unsteady, inviscid governing equations. A Schlieren system is employed to visualize the self-induced oscillations generated in flow field. The data of the shock motions are obtained from a high-speed video system. The detailed characteristics of the Mach disk oscillations and the resulting pressure variations are expatiated using the time dependent data of the Mach disk positions. The mechanisms of the self-induced oscillations are discussed in details based upon the experimental and computational results.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2001년도 춘계 학술대회논문집
• /
• pp.189-194
• /
• 2001

In this paper, non-reacting and reacting flowfields were computed using a preconditioned Navier-Stokes solver. The preconditioning technique of Merkle et al. and TVD scheme or Chakravarthy and Osher was employed and the results obtained using developed code have a good agreement with the previous results and experimental data. The preconditioned Wavier-Stokes equation set with low Reynolds number $\kappa-\epsilon$ equation and species continuity equations, are discretized with strongly implicit manner and time integrated with LU-SSOR scheme. For the purpose of treating unsteady problem the duel-time stepping scheme was employed. For the validation of the code in incompressible flow regime, steady driven square cavity flow was considered and calculation result shows reasonably good agreement with the result of incompressible code. Shock wave/boundary layer interaction problem was considered to show the shock capturing performance of preconditioned-TVD scheme. To validate unsteady flow, acoustic oscillation problem was calculated, and supersonic premix flame of $H_2$-air reaction problem which is calculated with turbulence model, 9-species/18-reaction step reaction model, shows reasonable agreement with the previous results. As a result, the preconditioning method has an advantage to calculate incompressible and compressible flow through one code and preconditioned solver easily developed from standard compressible code with minor efforts. But additional computational time and computer memory is required due to preconditioning matrix.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 1998년도 춘계 학술대회논문집
• /
• pp.1-14
• /
• 1998

Underwater explosion properties for TNT, an ideal explosive, and DXD-04, a nonideal explosive, were numerically modeled with a one-dimensional Lagrangian hydrodynamic code. The equation of state parameters for detonation products for TNT and DXD-04 were obtained from the BKW code, assuming complete reaction. Burn of TNT was modeled by using the Chapman-Jouguet(CJ) volume burn technique, a programmed-burn technique, assuming instantaneous detonation reaction. Burn of DXD-04 was modeled by using the same technique and by using the reaction rate calibrated from two-dimensional steady-state detonation experiments. The calculations for TNT reproduced the experimental peak pressure of the shock wave propagating through water with an error of $3.0\%$ and the experimental oscillation period of the bubble formed of detonation products with an error of $2.3\%$. For DXD-04, the CJ volume burn technique could not reproduce the experimental observations. When the reaction rate calibrated from two-dimensional steady-state detonation experimental data, the calculated peak pressure was slightly higher by $7.3\%$ than the experimental data, but the calculated shock profile was in good agreement. The bubble period was reproduced with an error of $1.8\%$. These results demonstrated that underwater explosion properties for an ideal explosive can be predicted by using a programmed burn technique, and that, however, those for a nonideal explosive can be predicted only when a well-calibrated reaction rate is used.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2003년도 추계학술대회
• /
• pp.508-513
• /
• 2003

Experiments are performed to investigate the detailed structure of underexpanded twin jet impinging on a perpendicular flat plate. The major parameters, such as nozzle operating pressure and nozzle spacing, are varied to create different jet flow fields resulted from the complicated interactions of the twin jets. From the surface pressure measurements and shadowgraphs taken by schlieren optical system, the jet structure is strongly dependent on the nozzle operation pressure and the spacing. The results obtained show that the closer nozzle spacing may induce to decrease the diameter of the Mach disk within the first shock cell in the underexpanded twin jet. With the increasing nozzle operating pressure and decreasing the nozzle spacing, a new shock wave appears at the entrainment region between the two jets, due to the enhancement of mixing effect of the both jets. The closer nozzle spacing makes the overall impinging pressure level higher, while severe pressure oscillation along the axis of symmetry. Furthermore it is recommended the wider spacing to obtain higher thrust under the present experimental conditions.