• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2007년도 춘계학술대회논문집
• /
• pp.928-933
• /
• 2007

In this research, we investigated active vibration control based on wave-viewpoint using the longitudinal wave separation method. The control strategy is the one of active vibration control technique for generating vibration reduced zone and uses wave information including the directivity as the cost function. In order to get the wave information from the measured values, we proposed and examined the time-domain longitudinal wave separation method proper to real time application like active vibration control. Using the proposed method, we examine the performance and feasibility of active vibration control based wave view-point through the simulation. The related experimental verification and application is going to be expected in a near future.

• 대한기계학회논문집
• /
• 제18권4호
• /
• pp.933-945
• /
• 1994

A shock-wave in a supersonic flow can be theoretically determined by a given pressure ratio at upstream and downstream flowfields, and then the obtained shock-wave is stable in its position. Under the practical situation in which the shock-wave interacts with the boundary layer along a solid wall, it cannot, however, be stable even for the given pressure ratio being independent of time and oscillates around a time-mean position. In the present study, oscillations of a weak normal shock-wave in a supersonic diffuser were measured by a Line Image Sensor(LIS), and they were compared with the data of the wall pressure fluctuations at the foot of the shock-wave interacting with the wall boundary layer. LIS was incorporated into a conventional schlieren optical system and its signal, instantaneous displacement of the interacting shock-wave, was analyzed by a statistical method. The results show that the displacement of an oscillating shock-wave increase with the upstream Mach number and the dominant frequency components of the oscillating shock-wave are below 200 Hz. Measurements indicated that shock-wave oscillations may not entirely be caused by the boundary layer separation. The statistical properties of oscillations appeared, however, to be significantly affected by shock-induced separation of turbulent boundary layer.

• 한국컴퓨터그래픽스학회논문지
• /
• 제25권4호
• /
• pp.9-16
• /
• 2019

본 논문에서는 대용량 비디오 영상에서 오토인코더를 이용하여 파랑 전파시 수리동역학적 장면만을 분리하는 방법에 대해 소개한다. 연안에서 센서를 이용한 파랑의 직접적 관측의 어려움으로 인해 비디오 영상을 이용한 입자 추적, 옵티컬 플로우 등의 이미지 분석 방법이 주로 활용되고 있다. 하지만 이미지 분석 방법은 주변광 및 기상상태 등 외부 요인에 의한 영향으로 파랑에 대한 정확한 분석에 어려움이 있다. 제안하는 방법은 비디오 영상으로부터 주변광의 영항을 최소화하고, 순수 파랑 전파시 파랑의 움직임 만을 분리하여 수리동역학적 장면을 추출한다. 실제 해역 및 수리 모형 실험에서 촬영된 비디오 영상에 제안하는 방법을 적용하여 원본 영상으로부터 주변광에 의한 영향과 배경을 잘 분리하여 파랑 전파에 따른 수리동역학적 파랑 이동 장면이 잘 추출되었음을 시각적으로 확인하였다. 또한 변분 오토인코더의 잠재표현 학습을 통해 얻은 원본 비디오 영상에 대한 잠재 표현은 주변광과 배경 요인에 의해 지배적으로 결정되는 반면, 파랑 이동 장면은 해당 요인에 관계없이 독립적으로 잘 표현되는 것을 알 수 있었다.

• 한국해안·해양공학회논문집
• /
• 제25권5호
• /
• pp.285-290
• /
• 2013

선형과 천해 edge wave로 구분되는 이들의 거동을 더 잘 이해하기 위해 비교하였다. 본 연구에서는 변수분리법을 사용하여, Ursell (1952)이 해의 유도과정 없이 제시한, 선형 edge wave의 해를 얻었다. 천해 edge wave는 비록 천해방정식으로부터 유도되지만 분산특성을 갖는다. 완만한 해저경사의 경우, 천해 파형은 선형 파형과 거의 같게 되고 천해 파형은 다루기가 쉬운 장점이 있다. Gaussian 분포형태의 이동체에 의해 생성되는 edge wave를 계산하기 위해 천해 고유파형으로 전개한 해를 구성하였고, 이에 대한 결과를 제시하고 특성을 기술하였다.

• 한국전산유체공학회지
• /
• 제2권2호
• /
• pp.59-72
• /
• 1997

A numerical model is constructed to simulate the interactions of oblique shock wave / turbulent boundary layer on a strongly heated wall. The heated wall temperature is two times higher than the adiabatic wall temperature and the shock wave is strong enough to induce boundary layer separation. The numerical diffusion in the finite volume method is reduced by the use of a higher order convection scheme(UMIST scheme) which is a TVD version of QUICK scheme. The turbulence model is Chen-Kim two time scale model. The comparison of the wall pressure distribution with the experimental data ensures the validity of this numerical model. The effect of strong wall heating enlarges the separation region upstream and downstream. In order to eliminate the separation, wall suction is applied at the shock foot position. The bleeding slot width is about same as the upstream boundary layer thickness and suction mass flow is 10% of the flow rate in the upstream boundary layer. The final configuration of the shock reflection pattern and the wall pressure distribution approach to the non-viscous value when wall suction is applied.

• Structural Engineering and Mechanics
• /
• 제87권2호
• /
• pp.165-172
• /
• 2023

This paper presents a novel method for modeling elastic wave propagation in long beams. The proposed method derives a solution for the transient transverse displacement of the beam's neutral axis without assuming the separation of variables (SV). By mapping the governing equation from the space domain to the frequency domain using Fourier transformation (FT), the transverse displacement function is determined as a convolution integral of external loading functions and a combination of trigonometric and Fresnel functions. This method determines the beam's response to general loading conditions as a linear combination of the analytical response of a beam subjected to an abrupt localized loading. The proposed solution method is verified through finite element analysis (FEA) and wave propagation patterns are derived for tone burst loading with specific frequency contents. The results demonstrate that the proposed solution method accurately models wave dispersion, reduces computational cost, and yields accurate results even for high-frequency loading.

• International Journal of Naval Architecture and Ocean Engineering
• /
• 제7권5호
• /
• pp.785-794
• /
• 2015

To obtain low resistance and high efficiency energy-saving ship, minimum total resistance hull form design method is studied based on potential flow theory of wave-making resistance and considering the effects of tail viscous separation. With the sum of wave resistance and viscous resistance as objective functions and the parameters of B-Spline function as design variables, mathematical models are built using Nonlinear Programming Method (NLP) ensuring the basic limit of displacement and considering rear viscous separation. We develop ship lines optimization procedures with intellectual property rights. Series60 is used as parent ship in optimization design to obtain improved ship (Series60-1) theoretically. Then drag tests for the improved ship (Series60-1) is made to get the actual minimum total resistance hull form.

• Journal of Mechanical Science and Technology
• /
• 제14권4호
• /
• pp.448-455
• /
• 2000

The bow wave breaking and the viscous interaction of stern wave are studied by simulating the free-surface flows. The Navier-Stokes equation is solved by a finite difference method in which the body-fitted coordinate system, the wall function and the triple-grid system are invoked. After validation, the calculations are extended to turbulent flows. The wave elevation at the Reynolds number of $10^4$ is much less than that at $10^6$ although the Froude number is the same. The numerical appearance of the sub-breaking waves is qualitatively supported by experimental observation. They are also applied to study the stern flow of S-103 for which extensive experimental data are available. Although the interaction between separation and the stern wave generation are not yet clear, the effects of the bow wave on the development of the boundary layer flows are concluded to be significant.

• 한국해안해양공학회지
• /
• 제4권3호
• /
• pp.139-145
• /
• 1992

본 논문에서는 2차원 수리모형실험시 인사파와 반사파를 분리할 수 있는 기법에 대해서 연구하였다. 계측오업의 제곱의 합을 최소화하는 방법을 이용하여 입, 반사파를 분리하는 기법을 체계적으로 수식화하였다. 이 분리기법은 규칙 및 불규칙 파낭조건에 대해서 적용이 가능하다. 본 방법의 타당성 및 적용성을 파악하기 위한 규칙 및 불규칙파에 대한 수치실험결과, 계측오차가 없는 경우는 거의 완벽하게 분리가 가능하며, 계측오차의 정도가 입사파고의 30% 정도일 경우에도 좋은 결과를 제시하는 것을 알 수 있었다. 또한 수리실험을 통한 실제상황으로의 적용성 검토도 수행하였다.

• 한국가시화정보학회지
• /
• 제8권3호
• /
• pp.56-62
• /
• 2010

The interaction patterns between shock wave and boundary layer in a rocket nozzle are mainly classified into two categories, FSS(Free Shock Separation) and RSS(Restricted Shock Separation), both of which are associated with the thrust characteristics as well as side loads of the engine. According to the previous investigations, strong side loads of the engine are produced during the period of transition from FSS to RSS or vice versa. The present work aims at investigating the unsteady behavior of the separation shock waves in a two-dimensional supersonic nozzle, using experimental method and CFD. Schlieren optical method was employed to visualize the time-mean and time-dependent shock motions in the nozzle. The unsteady, compressible N-S equations with SST K-$\omega$ turbulence closure were solved using a fully implicit finite volume scheme. The results obtained show the separation shock motions during the transition of the interaction pattern.