• 한국자동차공학회논문집
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• 제12권1호
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• pp.114-121
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• 2004

Frictional heating in brakes causes thermoelastic distortion of the contacting bodies and hence affects the contact pressure distribution. The resulting thermo-mechanical coupling can cause thermoelastic instability (TEI) if the sliding speed is sufficiently high, leading to non-uniform heating called hot spots and low frequency vibration known as hot judder. The vibration of brakes to the known phenomenon of frictionally-excited thermoelastic instability is estimated studying the interface temperature and pressure evolution with time. A simple model has been considered where a layer with half-thickness$\alpha$slides with speed V between two half-planes which are rigid and non-conducting. The advantage of this properlysimple model permits us to deduce analytically the critical conditions for the onset of instability, which is the relation between the critical speed and the growth rate of the interface temperature and pressure. Symmetrical component of pressure and temperature distribution at the layer interfaces can be more unstable than antisymmetrical component. As the thickness $\alpha$ reduces, the system becomes more apt to thermoelastic instability. For perturbations with wave number smaller than the critical$m_{cr}$ the temperature increases with m vice versa for perturbations with wave number larges than $m_{cr}$ , the temperature decreases with m.

• 한국항공우주학회지
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• 제33권7호
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• pp.18-25
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• 2005

본 연구에서는 뒷전, 전단류와 초기교란의 상호작용에 의한 불안정파의 생성 기제의 분석과 뒷전 산란현상을 고차의 전산공력음향학을 이용하여 모사하였다. 수치적 알고리즘은 Hybrid 기법에 기초하였으며, Simple Linearized Euler Equation과 Full Linearized Euler Equation의 결과를 비교를 통해 정상류 구배항이 불안정파의 생성에 중요한 역할을 함을 볼 수 있었다. 또한 Full Navier-Stokes Equation을 이용한 결과와 비교함으로써, Full Linearized Euler Equation은 뒷전의 초기 근접장에서 불안정파를 해석하는데 있어서 Full Navier-Stokes Equation 보다 효율적임을 알 수 있다.

• 해양환경안전학회지
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• 제23권3호
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• pp.320-329
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• 2017

In this research, we have calculated characteristics of wave-piercing high-speed planing hull, by using a RANS solver and overset grid method, for comparing with experimental measurements of that and simulating with several appendages, since the computed results of commercial CFD code look reasonable for the prediction of the performances of planing hulls on calm water in planing conditions. As a result, it is confirmed that the dynamic instability phenomena in pitch and heave motions (porpoising) occurred after a certain $Fn_V$, and effectively suppressed using some of appendages, especially the 0.5L spray rail is suppressed to 24-55 % in the pitch motion and 33-55 % in the heave motion. In spray phenomenon, 1L hard chine suppress spray effectively and it is effective to set the angle of appendages to be less than $0^{\circ}$ in order to suppress wave.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.294-299
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• 2012

연소기 내의 연소반응 촉진 및 연소불안정성 해결의 단초를 제공하기 위해, 정상초음파가 개재된 프로판/공기 예혼합화염의 구조거동을 고찰하는 연구를 수행하였다. 화염대의 구조 변이를 가시화하기 위해 슐리렌 기법을 이용하였으며, 당량비에 따른 화염선단의 형상 및 화염 전파속도의 변화를 확인할 수 있었다. 정상초음파는 화염선단을 찌그러뜨렸고, 난류 화염으로의 천이를 가속시켰다.

• Journal of applied mathematics & informatics
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• 제42권1호
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• pp.105-121
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• 2024

We consider incompressible, inviscid, stratified shear flows in β plane. First, we obtained an unbounded instability region intersect with semi-ellipse region. Second, we obtained a bounded instability regions depending on Coriolis, stratification parameters and basic velocity profile. Third, we obtained a criterion for wave stability. This has been illustrated with standard examples. Also, we obtained upper bound for growth rate.

• International Journal of Aerospace System Engineering
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• 제2권2호
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• pp.58-61
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• 2015

Combustion instability in solid rocket motors is a long-term open problem since the first rockets were used. Based on the numerous previous studies, it is known that the limit cycle amplitude is one of the key characteristics of the nonlinear combustion instability in solid rocket motors. Flandro's extended energy balance corollary, aims to predict the limit cycle amplitude of complex, nonlinear pressure oscillations for rockets or air-breathing engines, and leads to a precise assessment of nonlinear combustion instability in solid rocket motors. However, based on the comparison with experimental data, it is revealed that the Flandro's method cannot accurately describe such a complex oscillatory pressure. Thus in this work we make modifications of the nonlinear term in the nonlinear wave equations which represents the interaction of different modes. Through this modified method, a numerical simulation of the cylindrical solid rocket has been carried out, and the simulated result consists well with the experimental data. It means that the added coefficient makes the nonlinear wave growth equations describe the experimental data better.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.232-235
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• 2007

A comprehensive numerical study was carried out to identify the on-set condition of the cell structures of oblique detonation waves (ODWs). Mach 7 incoming flow was considered with all other flow variables were fixed except the flow turning angles varying from 35 to 38. For a given flow conditions theoretical maximum turning angle is $38.2^{\circ}$ where the oblique detonation wave may be stabilized. The effects of grid resolution were tested using grids from $255{\times}100$ to $4,005{\times}1,600$. The numerical smoked foil records exhibits the detonation cell structures with dual triple points running opposite directions for the 36 to 38 turning angles. As the turning angle get closer to the maximum angle the cell structures gets finer and the oscillatory behavior of the primary triple point was observed. The thermal occlusion behind the oblique detonation wave was observed for the $38^{\circ}$ turning angle.

• 한국강구조학회 논문집
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• 제29권6호
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• pp.401-410
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• 2017

본 연구에서는 긴장재로 계류된 해중 터널에서 긴장재의 느슨해짐에 따른 동적 불안정 거동에 대해 다룬다. 해중 터널의 설계는 파랑 및 조류 등 유체력에 의해 지배받는다. 특히 시간에 따라 지속적으로 크기 및 작용방향이 변하는 파랑은 해중 터널의 동적 거동을 직접적으로 야기하게 되는데, 파랑에 의한 부유 튜브의 운동은 계류선 내력의 동적 변동을 유발하게 되고, 이 힘의 변화는 계류선의 강도설계 뿐 만 아니라 피로 설계에도 직접적인 영향을 미친다. 파랑에 의한 터널의 운동이 극심할 경우, 계류선의 장력은 모두 소실될 수 있는데, 이 때 계류선이 느슨해짐에 따라 일시적으로 부유 터널의 운동에 대한 저항성이 사라져 동적 불안정 거동이 유발 될 수 있다. 이에 본 연구에서는 유체-구조동역학 해석기법을 통해 해중 터널 긴장재의 느슨해짐 발생 시 부유 튜브의 동적 불안정 거동에 대해 분석하였다. 특히 해중터널의 중요 설계 인자인 흘수, 부력-자중 비율(Buoyancy-Weight Ratio, BWR), 긴장재 기울임이 동적 불안정 거동에 미치는 영향에 대해 분석하였다.

• 대한기계학회논문집
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• 제13권1호
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• pp.161-169
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• 1989

본 연구의 목적의 하나는 기본 유동장과 온도장의 비평행성을 고려함으로써 등온 수직 원통표면 바깥에서의 자연대류 유동의 파형 불안정성에 대한 안정성 문제를 구성하는 것이다. 다음에는 기본 유동양들의 평행성을 고려한 단순화 가정하에 수치해석을 수행하여 안정성 특성에 대한 원통 곡률의 영향을 정성적으로 검토하는 것이다.

• Structural Engineering and Mechanics
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• 제14권4호
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• pp.455-472
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• 2002

The paper involves the study on the elastic and elasto-plastic stress wave propagation in the 1-D and 2-D solid media. The Smooth Particle Hydrodynamics equations governing the elastic and elasto-plastic large deformation dynamic response of solid structures are presented. The proposed additional stress points are introduced in the formulation to mitigate the tensile instability inherent in the SPH approach. Both incremental rate approach and leap-frog algorithm for time integration are introduced and the new solution algorithm is developed and implemented. Two examples on stress wave propagation in aluminium bar and 2-D elasto-plastic steel plate are included. Results from the proposed SPH approach are compared with available analytical values and finite element solutions. The comparison illustrates that the stress wave propagation problems can be effectively solved by the proposed SPH method. The study shows that the SPH simulation is a reliable and robust tool and can be used with confidence to treat transient dynamics such as linear and non-linear transient stress wave propagation problems.