• 대한기계학회논문집B
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• 제30권12호
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• pp.1155-1163
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• 2006

Calculation was carried out for phase velocity and deformation wave decay in a layer of viscoelastic material fixed tightly on the solid substrate. Analysis has been performed regarding the inner structure of the wave, i.e., the proportions between the vertical and horizontal displacements and their profiles. The wave characteristics depend strongly on media compressibility factor. The effect of viscous losses on parameters of the main oscillation mode was studied in detail. Results were compared with the model of coating with local deformation. A new experimental approach was made in order to measure such wave properties of a compliant coating as the dependency of deformation wave velocity on frequency and decay factor was made. The method for estimation of coating parameters enabling the drag reduction in turbulent flow was then refined.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.758-759
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• 2010

본 논문에서는 포물선 형상의 팽창부로 설계된 이차원 노즐(M=3)에 톱니 형태의 대칭 및 비대칭 파동 채널을 교대로 설치하여 원형 음속 노즐에서 발생하는 추력과의 추력편차를 측정함으로써, 두 파동 벽면 내에서 일어나는 조파저항의 공진현상을 실험적으로 확인하였다.

• 대한기계학회논문집B
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• 제27권5호
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• pp.655-667
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• 2003

Turbulent flow over a fully-developed wavy channel is investigated by the nonlinear $k-\varepsilon-f_\mu$ model of Park et al.⁽¹⁾ The Reynolds number is fixed at $Re_{b}$ = 6760 through all wave amplitudes and the wave configuration is varied in the range of $0\leq\alpha/\lambda\leq0.15$ and $0.25\leq{\lambda}/H\leq4.0$. The predicted results for wavy channel are validated by comparing with the DNS data of Maa$\beta$ and Schumann⁽²⁾ The model performance Is shown to be generally satisfactory. As the wave amplitude increases, it is found that the form drag grows linearly and the friction drag is overwhelmed by the form drag. In order to verify these characteristics, a large eddy simulation is performed for four cases. The dynamic model of Germane et al.⁽³⁾ is adopted. Finally, the effects of wavy amplitude on separated shear layer are scrutinized.

• 한국분무공학회지
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• 제1권2호
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• pp.57-65
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• 1996

Breakup models are evaluated using the experimental drop trajectory ill this study. The experimental conditions corespond to Weber # 56, 260, 463. Computations are carried out using a modified KIVA-II program with 2 different breakup submodel(TAB and Wave breakup model) and dynamic drag model which the drag coefficient changes dynamically with distortion parameter. Results show that computation with wave breakup model represents the experimental drop trajectory better than that with TAB submodel. And result with wave breakup model shows similar breakup pattern to experimental breakup process. It is thought that in wave breakup model the small drops are shed from the parent drop throughout parcel lifetime such thai this modelling represents the real breakup process well.

• 한국해안해양공학회지
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• 제5권1호
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• pp.25-38
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• 1993

해양구조물의 케이블 반응 분석을 위한 다방향 파람 스펙트라의 수치모델이 조사되었다. 여러 형태의 전파모델을 파랑으로 인한 물입자의 흐름과 계류시스템을 예측하기 위해 사용하였다. 케이블에 작용하는 수동역학적 파력은 케이블의 경사에 평행한 방향과 접선방향에서의 항력과 관성력을 고려한 Morison 공식에 의해 평가되었다. 변위와 속도, 궤적, 위상면의 반응, 그리고 장력을 고려한 다방향 불규칙 파랑의 수치해석에 의하여 부체의 tether pc와 anchor point에서 계류시스템 케이블의 반응을 나타내었다. 서로 다른 항력 계수와 다양한 유의 파고, 그리고 선택된 파랑계수들이 이 분석에 고려되었다. 예제에서 고려된 특정 시스템을 통하여 파랑의 전파함수계수와 항력계수 뿐만 아니라 파랑의 주기와 높이가 케이블-부체시스템의 동적반응에 중요한 영향을 미침을 알 수 있었다.

• 대한기계학회논문집B
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• 제40권12호
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• pp.785-792
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• 2016

본 연구에서는 NACA0012 천음속 익형 유동에 있어 비평형 응축이 항력 발산 마하수 $M_D$에 미치는 영향을 TVD 유한 차분법을 사용하여 연구하였다. 받음각 ${\alpha}$가 동일한 경우, 정체점 상대습도 ${\phi}_0$가 높을수록 충격파 직전의 최대 마하수 $M_{max}$는 작게 되고 초음속 영역의 크기도 적게 된다. 주류 마하수 $M_{\infty}$, 정체점 상대습도 ${\phi}_0$ 및 정체온도 $T_0$가 동일한 경우 받음각 ${\alpha}$가 클수록 비평형 응축영역 길이 ${\Delta}_z$은 짧게 된다. 한편, 주류 마하수 $M_{\infty}$와 받음각 ${\alpha}$가 동일한 경우 정체점 상대습도 ${\phi}_0$가 높을수록 조파저항의 감소 때문에 항력계수 $C_D$는 적어진다. $M_D$는 ${\alpha}$가 동일한 경우 ${\phi}_0$가 클수록 크게 되며, ${\phi}_0$가 동일한 경우는 ${\alpha}$가 클수록 $M_D$는 적게 된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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• pp.299-302
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• 2007

The aerodynamics of a projectile overtaking a moving shock wave is analyzed using a chimera scheme. The flow field characteristics for various shock wave Mach number and projectile masse are investigated. the unsteady forces acting on the projectile for both supersonic and impossible overtaking conditions are computed in order to analyze the aerodynamic characteristics of the projectile. It is seen that the projectile Mach number significantly affects the flow fields for both supersonic and impossible overtaking. Unsteady drag is influenced by the overtaking conditions. The unsteady drag coefficient is the highest for the impossible overtaking condition.

• International Journal of Naval Architecture and Ocean Engineering
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• 제11권1호
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• pp.510-520
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• 2019

To investigate the morphology characteristics of air layer in the air cavity, a numerical method with the combination of RANS equations and VOF two-phase-flow model is proposed for a plate with air cavity. Based on the model above, the dynamic and developmental process of air layer in the air cavity is studied. Numerical results indicate that the air layer in the plate's air cavity exhibits the dynamic state of morphology and the wavelength of air layer becomes larger with the increasing speed. The morphology of air layer agrees with the Froude similarity law and the formation of the air layer is not affected by the parameters of the cavity, however, the wave pattern of the air layer is influenced by the parameters of the cavity. The stable air layer under the air cavity is important for the resistance reduction for the air layer drag reduction.

• 대기
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• 제17권3호
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• pp.231-240
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• 2007

The flow regimes of continuously stratified flow over a double mountain and the effects of a double mountain on wave breaking, upstream blocking, and severe downslope windstorms are investigated using a mesoscale numerical model (ARPS). According to the occurrence or non-occurrence of wave breaking and upstream blocking, three different flow regimes are identified over a double mountain. Higher critical Froude numbers are required for wave breaking and upstream blocking initiation for a double mountain than for an isolated mountain. This means that the nonlinearity and blocking effect for a double mountain is larger than that for an isolated mountain. As the separation distance between two mountains decreases, the degree of flow nonlinearity increases, while the blocking effect decreases. A rapid increase of the surface horizontal velocity downwind of each mountain near the critical mountain height for wave breaking initiation indicates that severe downslope windstorms are enhanced by wave breaking. For the flow with wave breaking, the numerically calculated surface drag is much larger than theoretically calculated one because the region with the maximum negative perturbation pressure moves from the top to the downwind slope of each mountain as the internal jump propagating downwind occurs.

• Ocean Systems Engineering
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• 제6권1호
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• pp.1-21
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• 2016

The global performance of the 5 MW OC4 semisubmersible floating wind turbine in random waves with or without steady/dynamic winds is numerically simulated by using the turbine-floater-mooring fully coupled dynamic analysis program FAST-CHARM3D in time domain. The numerical simulations are based on the complete second-order diffraction/radiation potential formulations along with nonlinear viscous-drag force estimations at the body's instantaneous position. The sensitivity of hull motions and mooring dynamics with varying wave-kinematics extrapolation methods above MWL(mean-water level) and column drag coefficients is investigated. The effects of steady and dynamic winds are also illustrated. When dynamic wind is added to the irregular waves, it additionally introduces low-frequency wind loading and aerodynamic damping. The numerically simulated results for the 5 MW OC4 semisubmersible floating wind turbine by FAST-CHARM3D are also extensively compared with the DeepCWind model-test results by Technip/NREL/UMaine. Those numerical-simulation results have good correlation with experimental results for all the cases considered.