• International Journal of Aeronautical and Space Sciences
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• 제15권4호
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• pp.345-355
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• 2014

This paper focuses on aerodynamic and inertial modeling of the propeller for its applications in flight dynamics analyses of a propeller-driven airplane. Unsteady aerodynamic and inertial loads generated by the propeller are formulated using the blade element method, where the local velocity and acceleration vectors for each blade element are obtained from exact kinematic relations for general maneuvering conditions. Vortex theory is applied to obtain the flow velocities induced by the propeller wake, which are used in the computation of the aerodynamic forces and moments generated by the propeller and other aerodynamic surfaces. The vortex lattice method is adopted to obtain the induced velocity over the wing and empennage components and the related influence coefficients are computed, taking into account the propeller induced velocities by tracing the wake trajectory trailing from each of the propeller blades. Aerodynamic forces and moments of the fuselage and other aerodynamic surfaces are computed by using the wind tunnel database and applying strip theory to incorporate viscous flow effects. The propeller models proposed in this paper are applied to predict isolated propeller performances under steady flight conditions. Trimmed level forward and turn flights are analyzed to investigate the effects of the propeller on the flight characteristics of a propeller-driven light-sports airplane. Flight test results for a series of maneuvering flights using a scaled model are employed to run the flight dynamic analysis program for the proposed propeller models. The simulations are compared with the flight test results to validate the usefulness of the approach. The resultant good correlations between the two data sets shows the propeller models proposed in this paper can predict flight characteristics with good accuracy.

• 대한토목학회논문집
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• 제31권4B호
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• pp.333-341
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• 2011

본 연구에서는 RANS를 지배방정식으로 하는 3치원 수치모의를 이용하여 댐 붕괴로 인한 3차원적인 흐름 특징이 지배하는 댐 직하류에서 댐 붕괴파의 전파 현상, 특히 홍수파의 비정상성과 불연속성, 홍수파와 그 빈사파의 영향, 상류 및 사류 흐름의 혼재, 마른 하도에서의 전파, 이동상 수로에서의 전파와 같은 복잡한 현상을 포함하는 홍수파의 전파를 해석하였다. 부분 댐 붕괴로 인한 홍수파의 전파 해석과 90${\circ}$ 만곡을 가지는 실험수로에서의 홍수파 전파 해석에서는, 2차원 천수방정식을 지배방정식으로 사용하는 수치모의의 한계점으로 지적되었던 댐 붕괴 지점에서의 급격한 수위 변화와 저수지에서의 수위 진동 현상을 제대로 모의할 수 있었다. 또한 댐을 경계로 상류와 하류의 지형이 평행하거나 상류가 높은 또는 하류가 높은 계단형의 이동상 수로에서의 홍수파의 전파 및 하상변동을 성공적으로 모의할 수 있었다.

• 물과 미래
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• 제20권4호
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• pp.285-294
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• 1987

본 연구는 댐파괴나 급격한 방류로부터 발생되는 홍수파가 하도내에서 사류의 흐름으로 나타날 때, 이를 해석하기 위한 수치모형을 개발한 것이다. 기본방정식으로서는 dynamic wave equation을 사용하였고 이식을 general Preissmann sceme에 의하여 유한차분화 시켰으며 fore-sweep algorithm에 의하여 해석하였다. 본 모형을 Buffalo-Creek flood의 경우에 적용하고 실측치 및 DAMBRK에 의한 계산 결과치와 비교검토하여 모형의 적용성을 입증하였다. 국내 효기댐의 경우에 대하여서는 파괴당시의 실측자료를 기초로한 유출수문곡선을 유도하였고 댐 하류부의 홍수파 전달양상을 해석하였다.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2000년도 춘계학술대회 논문집(Proceeding of the KOSME 2000 Spring Annual Meeting)
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• pp.36-44
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• 2000

In his study the simulation was carried out by simplifing and modeling dividing into fuel injectioin pump high pressure pipe and fuel injection valve in the fuel injection system of a low speed marine diesel engine. A computer simulation model was developed using the method of characteristics to analyze the unsteady flow in the fuel injection system considering cavitation and variation of fuel density and bulk modulus. Comparison was commenced between the calculated data and experimental data of pressure and injection quantity at the high pressure distributor in fuel injection system for the training ship "M/V hanara" the effects of the high pressure pipe length diameter plunger diameter nozzle openning pressure were also investigated by simulating results.g results.

• 한국콘텐츠학회:학술대회논문집
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• 한국콘텐츠학회 2011년도 춘계 종합학술대회 논문집
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• pp.465-466
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• 2011

이 연구는 일본식 배수공이 설치된 제방의 침투 흐름을 비정상 상태로 SEEP/W 모형을 사용하여 해석하고 모형의 적용성을 평가하기 위해 수행하였다. 수치모형의 적용성 평가를 위해 비정상 상태로 제방 침투에 대한 수리모형실험을 수행하였다. 제체 재료는 경상북도 구미시에 위치한 해평천의 제방 건설 현장의 재료를 사용하였고 일본식배수공은 굵은 골재와 부직포를 사용하여 실험실에 제방 축소 모형을 수조 내부에 제작하였다. 모형제방은 제방축조 방법과 유사하게 다짐을 하기 위해 흙을 쌓으면서 0.20 m 높이마다 다짐을 실시하였다. 다짐방법은 고무망치를 이용한 층다짐을 하였다. 제방 제외지에 0.55 cm/min의 속도로 수위를 증가하여 15분 간격으로 각 0.3 m, 0.4 m, 0.5 m 수위에 따른 비정상 상태의 위압계 측정을 수행하였다. SEEP/W 모형의 매개변수는 투수계수와 입도분포도, 불포화 함수특성곡선(값을 산정하기 어려움)이 있으며, 각 매개변수에 대한 민감도 분석을 수행하였다. SEEP/W 모형의 모의 결과는 수리모형실험 결과와 비교적 잘 일치함을 알 수 있었다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1716-1720
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• 2000

To develop the code of predicting flow-field and aeroacoustic noise by a electrical cable, a combined CFD-acoustic analogy approach is selected. The two-dimensional, unsteady, incompressible Reynolds-Averaged Navier-Stokes solver with a ${\kappa}{\omega}$, ${\kappa}{\omega}$ SST turbulence modeling is used to calculate the near-field around electrical cable. Near-field results are then coupled with two-dimensional Curle's integral formulation based upon Lighthill's acoustic analogy with an assumption of acoustic compactness. To validate this code, numerical results are compared with experimental data for a circular cylinder. The simulation shows an overprediction on acoustic amplitudes, but overally speaking, the spectrum pattern of sound pressure agrees well with experiment in an acceptable amount of error. In addition, various cross sections of a cable were selected and compared with each other in terms of drag and radiated noise.

• 오토저널
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• 제10권4호
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• pp.57-65
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• 1988

The study of unsteady gas exchange processes in the intake and exhaust systems of four-cylinder, four-stroke cycle internal combustion engine is described in this paper. The calculation model for the intake and exhaust systems is established and solved by the characteristic method for the equations defining these systems. A constant pressure theory is used for modeling branches of intake and exhaust manifolds. The relationship between the volumetric efficiency and the intake, exhaust pressure variation is clarified by simulation of these systems. It is found that the volumetric efficiency mainly depends on the intake pressure during the short period before the intake valves is closed, that the volumetric efficiency is influenced a little by intake chamber volume in the intake and exhaust system.

• 한국분무공학회지
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• 제22권2호
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• pp.55-61
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• 2017

This study has investigated the relationship between heat release fluctuations and the flow perturbations in a partially premixed gas turbine combustor using a commercial CFD code. Special focus of the current work is placed on the effect of equivalence ratio on the flame dynamics in a partially-premixed system. As the first step for this combustion dynamics study in the non-perfectly premixed combustor, flame behaviors are modeled and then compared with measured results under both steady and unsteady conditions. The calculated results of the flame transfer function with equivalence ratio fluctuation are found to well capture the main qualitative characteristics of the combustion dynamics for the partially-premixed flames.

• Journal of Mechanical Science and Technology
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• 제18권7호
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• pp.1196-1202
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• 2004

To evaluate the unsteady motion in laterally berthing maneuver, it is necessary to estimate clearly the magnitudes and properties of hydrodynamic forces acting on ship hull in shallow water. A numerical simulation has been performed to investigate quantitatively the hydrodynamic force according to water depth for Wigley model using the CFD (Computational Fluid Dynamics) technique. By comparing the computational results with the experimental ones, the validity of the CFD method was verified. The numerical solutions successfully captured some features of transient flow around the berthing ship. The transitional lateral force in a state ranging from the rest to the uniform motion is modeled by using the concept of circulation.

• Advances in Computational Design
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• 제6권1호
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• pp.43-53
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• 2021

Multi-stage pumps are the most popular pumps among various kinds of centrifugal pumps. Athorough review of different kinds of literature has led to the conclusion that there is a desperate need to increase the performance of the multi-stage centrifugal pump. Many investigators have put their efforts to increase the pump performance and also the work is being projected on various aspects of pump performance variables. To improve the multistage centrifugal pump performance by investigation, modification, and analysis many works of literature are available. For analysis, many researchers used the Navier-Stokes solver to create the three-dimensional unsteady turbulent flow numerical model with the standard k-ε turbulent equation. This paper mainly focuses on research related to the multi-stage centrifugal pump.