• 한국지반공학회논문집
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• 제15권6호
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• pp.45-55
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• 1999

파랑에 의한 불포화된 해저지반의 거동, 액상화와 전단파괴에 대한 연구이다. 불포화된 지반은 유체가 채워진 다공성 탄성체로 모델화 하였다. 유체의 흐름과 토립자의 변형은 Biot의 이론에 따른 지배방정식으로 나타내었다. 이 방정식은 준해석적 방법으로 풀어 불포화된 다층의 지반에 대하여 응력과 간극수압을 평가하였다 준해석적 방법은 기존의 해석방법과 달리 다층의 이방성 지반을 연속적으로 해석할 수 있다. 해석결과에 의하면, 지반의 포화도는 불포화된 다층의 지반에서 응력과 간극수압의 크기에 가장 큰 영향을 미치고 있는 것으로 나타났다. 또한, 해석결과를 토대로 지반의 액상화 발생과 전단파괴에 대한 검토를 실시하였으며, 그 결과 최대 전단파괴가 발생된 깊이가 최대 액상화 발생지역 보다 깊은 것으로 나타났다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.616-621
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• 2003

Fluid-elastic instability is believed to be a cause of the large-amplitude vibration and resulting rapid wear of heat exchanger tubes when the flow velocity exceeds a critical value. For sub-critical flow velocities, the random turbulence excitation is the main mechanism to be considered in predicting the long-term wear of steam generator tubes. Since flow-induced interactions of the tubes with tube supports in the sub-critical flow velocity can cause a localized tube wear, tube movement in the clearance between the tube and tube support as well as the normal contact force on the tubes by fluid should be maintained as low as possible. A simplified method is used for predicting fretting-wear damage of the double $90^{\circ}$U-bend tubes. The approach employed is based on the straight single-span tube analytical model proposed by Connors, the linear structural dynamic theory of Appendix N-1300 to ASME Section III and the Archard's equation for adhesive wear. Results from the presented method show a similar trend compared with the field data. This method can be utilized to predict the fretting-wear of the double $90^{\circ}$U-bend tubes in steam generators.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.1095-1100
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• 2003

Experimental studies on the aerodynamic coupling effect on natural frequencies, critical speed and flutter instability of DVD disks are investigated in this paper. The experimental results are compared with the theoretical analyses where the aerodynamic effects are represented in terms of elastic, lift and damping and stiffness components. The experiments are performed using a vacuum chamber and DVD disks rotating in vacuum, open and enclosure with several different gaps between disk and wall. The following three results are given. One is that the aerodynamic effect by the surrounding air reduces the natural frequencies and critical speeds of the vibration modes. The second is that natural frequency decreases as the disk-wall gap is decreased. Finally, it is shown that the disk vibration is reduced as the gap between the disk and the rigid wall decreases.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.677-683
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• 2002

The analytical and experimental studies on aerodynamic flutter instability of rotating disks in information storage devices are investigated. The theoretical analysis uses a fluid-structure model where the aerodynamic force on the rotating disk is represented in terms of lift and damping forces. Based on the analytical approach, it is shown that the backward natural frequency of the disk is equal to that of the case without aerodynamic effect at the flutter onset speed. In post-flutter regions, the natural frequencies are larger than those in vacuum conditions without aerodynamic effect. The analytical predictions on the natural frequencies of rotating disks with/without aerodynamic effect are experimentally verified using a vacuum chamber and ASMO optical disks.

• 대한기계학회논문집A
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• 제30권12호
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• pp.1588-1595
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• 2006

The stabilities of a pinned-pinned straight pipe conveying fluid are investigated by complexification-averaging method. The flow is assumed to vary harmonically about a constant mean velocity. Instability conditions of a governing equation are analytically obtained about parametric primary, secondary and combination resonances. The resulted stability conditions show that instabilities exist when the frequency of flow fluctuation is close to one and two times the natural frequency or to the sum of any two natural frequencies. In case that the fluctuated flow frequency is close to the difference of two natural frequencies, instabilities does not exist.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 추계학술대회논문집 II
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• pp.1207-1214
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• 2001

The paper deals with the computational approach in analysis and design of pantograph panhead strips of high-speed railway in aerodynamic and aeroacoustic concerns. Pantograph is an equipment such that the electric power is supplied from catenary system to train. Due to the nature of complexity in high-speed fluid flow, turbulence and downstream vortices result in the instability in the aerodynamic contact between panhead strips and catenary system, and consequently generate the considerable levels of flow-induced sound. In this paper, based on the preceding low speed wind-tunnel test and simulations, the aerodynamic and aeroacoustic characteristics in low speed are analyzed.

• 지질공학
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• 제32권4호
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• pp.643-659
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• 2022

최근 지중저장기술(예, 온실가스 심지층 처분, 인공지열저류층 발전 등)이 활발히 수행됨에 따라, 유체 주입과 저장부지 안정성 사이의 역학적 관계에 관한 정량적 이해의 중요성이 인지되고 있다. 지중 유체 주입은 공극압 및 지중응력 교란과 지층의 역학적 불안정성을 야기할 수 있어, 유체 주입에 대한 다공탄성 수치 모형 구축이 요구된다. 본 연구에서는 순차적인 COMSOL-PyLith-COMSOL 유체 주입-유발지진 다공탄성 수치 모사를 수행한다. 유한요소 상용 소프트웨어인 COMSOL을 이용해 단층에 가해지는 쿨롱 파괴 응력(CFS) 변화를 시간에 따라 추적하였고, CFS 변화량이 임계값(예, 0.1 MPa)을 초과할 경우, 모형의 정보(기하구조, 물성 등)를 유한요소 오픈소스 코드인 PyLith로 이동시키는 알고리즘을 구축했다. PyLith는 단층의 미끄러짐을 모사하고, 미끌림에 의한 변위장을 획득한다. 이후 변위장을 COMSOL로 이동시켜 지진에 의한 응력 및 표면 변위를 계산한다. 수치 모사 결과, 주입 기간 중엔 주입정 근거리에서 큰 변화(공극압, CFS 변화 등)를 보였고, 주입 종류 후에는 잔류 응력이 원거리 영역으로 확산하는 양상이 나타났다. 이는 주입 종료 후 지속적인 모니터링의 필요성을 제안한다. 또한, 단층과 주입층 물성(예, 투수계수, Biot-Willis 계수)에 따른 CFS 변화량 비교는 주입정 위치 선정 시 주입층 및 주변 지층에 대한 물성 파악이 중요함을 의미한다. 단층 미끄러짐 양에 따른 표면 변위 및 이암층에 가해지는 편차응력은 다양한 단층 미끌림 시나리오 설정의 필요성을 지시한다.

• 한국유체기계학회 논문집
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• 제20권2호
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• pp.53-62
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• 2017

In this paper, the effect of oil conditions in rotor dynamic behaviors of a FFRB (Fully-Floating Ring Bearing) is investigated. Through the characteristic of a FFRB has two films, it has several advantages such as less friction loss and better stability over a wide speed range. However, it is difficult to supply a oil to the inner film. Thus, turbocharger makers have been paid significant attention to the lubrication of a FFRB because of its importance. This work focuses on the influence of oil inlet pressure and temperature. The methodologies of computational simulation and experimental test were used to estimate the rotor dynamic behaviors. In experimental test, the single-scroll turbocharger for the 1.4L diesel engine was used. The results show that the oil inlet pressure and temperature will place considerable influence on the rotor response. Oil conditions affect RSR (Ring Speed Ratio) which is cause of sub-synchronous vibrations, which also cause of oil whirling and whip even a critical speed. At higher speed range, the phenomenon of self-excited vibrations which is cause of instability of fluid whirl is investigated through the orbit shapes that consist of small orbit and large amplitude orbit. It is shown that some performance of a FFRB can be controlled by the conditions of oil supply. Finally, it was revealed that the oil induced operating conditions will strongly affect the turbocharger rotor dynamics behaviors.

• 대한기계학회논문집
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• 제15권6호
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• pp.1861-1871
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• 1991

본 연구에서는 아직까지 연구가 미진한 내용 즉, 유속과 압력이 시간과 위치 의 함수인 유동특성과 파이프의 운동이 상호 연계되어 영향을 주는 일반적인 경우의 운동방정식을 유도하였고 단순지지된 직선 파이프를 모델로 설정하여 동적 안정성 (dynamic stability)과 진동응답을 수치적으로 고찰하였다.

• 한국해양공학회지
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• 제18권5호
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• pp.15-21
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• 2004

An edge tone is the discrete tone or narrow-band sound produced by an oscillating free shear layer, impinging on a rigid surface. In this paper, we present a 2-D edge tone to predict the frequency characteristics of the discrete oscillations of a jet-edge feedback cycle, using the finite difference lattice Boltzmann method (FDLBM). We use a modified version of the lattice BGK compressible fluid model, adding an additional term and allowing for longer time increments, compared to a conventional FDLBM, and also use a boundary fitted coordinates system. The jet is chosen long enough in order to guarantee the parabolic velocity profile of the jet at the outlet, and the edge consists of a wedge with an angle of ${\alpha}$ = 23. At a stand-off distance, the edge is inserted along the centerline of the jet, and a sinuous instability wave, with real frequency, is assumed to be created in the vicinity of the nozzle and propagates towards the downstream. We have succeeded in capturing very small pressure fluctuations, resulting from periodical oscillations of a jet around the edge. The pressure fluctuations propagate with the speed of sound. Its interaction with the wedge produces an non-rotational feedback field, which, near the nozzle exit, is a periodic transverse flow, producing the singularities at the nozzle lips.