• 대한기계학회논문집B
• /
• 제31권2호
• /
• pp.109-115
• /
• 2007

Airframe-integrated Scramjet engines of NASA Langley type consist of a compressor, a combustion chamber and a nozzle. When some disturbances occur in one module of the engine, its influences are propagated to other modules. In this study, it is investigated numerically how shock waves were caused by thermal choking in one module propagate upstream and how they influence adjacent modules. The calculations are carried out in 2-dimensional supersonic viscous flow model using explicit TVD scheme in generalized coordinates. The adverse pressure gradient caused by heat addition brings about separation of the wall boundary layers and formation of the oblique shock wave that proceed to upstream. This moving shock wave formed one module blocks the flow coming into the adjacent modules, which makes the modules unstarted.

• 한국지형학회지
• /
• 제23권1호
• /
• pp.129-140
• /
• 2016

Camera monitoring data for 5 years from January 2009 to January 2014 are analyzed to investigate changes in beach erosion on Sangju, Gujora and Haeundae beaches on the South sea and Jungmun beach on the south shore of Jeju Island. The data show the time series of beach area changes obtained from digital orthoimages rectified from oblique images taken near the beaches by cameras. Each beach has different sediment sizes and shapes, but faces the South and is eroded mainly during Typhoons. However, each beach often responds differently to the same Typhoon, and some beaches outside the influence of the Typhoon are also eroded. This study shows that high frequency data of beach area changes obtained from cameras can effectively analyze the seasonal changes in beach area.

• 대한기계학회논문집
• /
• 제9권2호
• /
• pp.158-173
• /
• 1985

본 연구에서는 상호작용상류의 난류경계층에 분출을 가해서 경계층을 불안정 화시키고 이 불안정화된 난류경계층과 사각입사충격파와의 상호작용을 실험적으로 연 구하였다. Squire-Smith와는 다른 실험모형의 새로운 형태를 제시하였고 상호작용영 역에서 경계층의 압력분포 및 속도분포를 측정해서 충격파반사의 형태를 밝혔다.

• 에너지공학
• /
• 제21권3호
• /
• pp.237-242
• /
• 2012

이 연구에서는 초음속 연소에서 발생하는 열폐색의 다양한 현상을 규명하기 위해 확대 축소 노즐 내부에서 열폐색에 의해 형성되는 2차원의 초음속의 비정상 유동장에 대한 수치해석 결과를 제시한다. 열폐색에 의해 야기되는 이동 충격파를 수치계산하기 위해 TVD 스킴을 이용하며, 노즐의 확대부의 일정영역에 가열을 통하여 열폐색이 발생할 수 있는 조건을 형성하고, 이 때 발생하는 천이현상을 분리부가 있는 경우와 없는 경우에 대해 불시동현상 발생속도, 비추력의 불안정성 등을 통해 비교, 설명한다. 분리부가 있는 경우가 없는 경우에 비해 열폐색에 의해 발생한 경사 충격파가 느린 속도로 상류측으로 이동하여 분리부의 설치가 엔진 불시동의 지연효과가 있음을 제시하였다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
• /
• pp.75-78
• /
• 2004

Various jet engines (Turbine engine family and RAM Jet engine) have been developed for high speed aircrafts. but their application to hypersonic flight is restricted by principle problems such as increase of total pressure loss and thermal stress. Therefore, the development of next generation propulsion system for hypersonic aircraft is a very important subject in the aerospace engineering field, SCRAM Jet engine based on a key technology, Supersonic Combustion. is supposed as the best choice for the hypersonic flight. Since Supersonic Combustion requires both rapid ignition and stable flame holding within supersonic air stream, much attention have to be given on the mixing state between air stream and fuel flow. However. the wider diffusion of fuel is expected with less total pressure loss in the supersonic air stream. So. in this study the direction of fuel injection is inclined 30 degree to downstream and the total pressure of jet is controlled for lower penetration height than thickness of boundary layer. Under these flow configuration both streams, fuel and supersonic air stream, would not mix enough. To spread fuel wider into supersonic air an aerodynamic force, baroclinic torque, is adopted. Baroclinic torque is generated by a spatial misalignment between pressure gradient (shock wave plane) and density gradient (mixing layer). A wedge is installed in downstream of injector orifice to induce an oblique shock. The schlieren optical visualization from side transparent wall and the total pressure measurement at exit cross section of combustor estimate how mixing is enhanced by the incidence of shock wave into supersonic boundary layer composed by fuel and air. In this study non-combustionable helium gas is injected with total pressure 0.66㎫ instead of flammable fuel to clarify mixing process. Mach number 1.8. total pressure O.5㎫, total temperature 288K are set up for supersonic air stream.

• 해양환경안전학회지
• /
• 제25권4호
• /
• pp.489-497
• /
• 2019

거친 해상 조건에서 운항하는 선박은 파도와의 상대운동으로 인해 슬래밍 하중에 노출된다. 특히 선수가 자유수면으로 입수하는 과정에서 선체부는 일시적으로 큰 슬래밍 충격하중을 받게된다. 일반적으로 대형 컨테이너선박의 경우, 큰 플레어를 가지는 특징이 있으며, 이로 인해 플레어 슬래밍 충격하중으로 인한 구조적 손상이 발생할 수 있다. 본 연구에서는 슬래밍 수치시뮬레이션을 위해 먼저 신뢰할 만한 실험결과와의 비교검증을 수행하였으며, 선수 및 사파에서 선수플레어 슬래밍 하중을 추정하였다. 그 결과 슬래밍 하중이 발생되는 위치는 0.975st이며, 최대 충격 하중은 선수파 조건에서 약 475kPa임을 확인하였다.

• 한국해양공학회지
• /
• 제27권3호
• /
• pp.61-66
• /
• 2013

This paper presents the results of finite element simulations of elastic wave propagation in an underwater steel plate and the verification of a proposed method utilizing elastic wave-based damage detection. For the simulation and verification, we carried out the following procedures. First, three-dimensional finite element models were constructed using a general purpose finite element program. Second, two types of damages (mechanical defects and deteriorations) were applied to the underwater steel plate and three parameters (defect location, defect width, and depth) were considered to adjust the severity of the applied damages. Third, elastic waves were generated using the oblique incident method with a Gaussian tone burst, and the response signals were obtained at the receiving point for each defect or deterioration case. In addition, the received time domain signals were analyzed, particularly by measuring the magnitudes of the maximum amplitudes. Finally, the presence and severity of each type of damage were identified by the decreasing ratios of the maximum amplitudes. The results showed that the received signals for the models had the same global pattern with minor changes in the amplitudes and phases, and the decreasing ratio generally increased as the damage area increased. In addition, we found that the defect depth was more critical than the width in the decrease of the amplitude. This mainly occurred because the layout of the depth interfered with the elastic wave propagation in a more severe manner than the layout of the width. An inverse analysis showed that the proposed method is applicable for detecting mechanical defects and quantifying their severity.

• 대한기계학회논문집B
• /
• 제27권10호
• /
• pp.1464-1471
• /
• 2003

In order to investigate the flows with shock wave in branch, 108$^{\circ}$ elbow and T-junction of the IRWST system of standard Korean nuclear reactor, detail time dependent behaviors of unsteady flow with shock wave, vortex and so on are obtained by numerical method using compressible three-dimensional Navier-Stokes equations. At first, the complex flow including the incident and reflected shock waves, vortex and expansion waves which are generated at the corner of T-junction is calculated by the commercial code of FLUENT6 and is compared with the experimental result to obtain the validation of numerical method. Then the flow fields in above mentioned units are analyzed by numerical method of [mite volume method. In numerical analysis, the distributions of flow properties with the moving of shock wave and the forces acting on the wall of each unit which can be used to calculate the size of supporting structure in future are calculated specially. It is found that the initial shock wave of normal type is re-established its type from an oblique one having the same strength of the initial shock wave at the 4 times hydraulic diameters of downstream from the branch point of each unit. Finally, it is turned out that the maximum force acting on the pipe wall becomes in order of the T-junction, 108$^{\circ}$ elbow and branch in magnitude, respectively.

• 한국인터넷방송통신학회논문지
• /
• 제10권1호
• /
• pp.33-38
• /
• 2010

본 논문은 유전률 ${\epsilon}_1$과 ${\epsilon}_2$로 구성된 주기적인 유전체 층을 사용하여 밀리미터 주파수 대역의 주파수 선택 반사기를 설계할 수 있음을 분석하였다. 임의의 각도에서 입사한 밀리미터파에 대하여 유전률 ${\epsilon}_1$, ${\epsilon}_2$와 주기적인 구조를 구성하는 변수들을 적합하게 선택함으로써 원하는 주파수의 밀리미터파를 전반사시키는 반사기 설계가 가능함을 보였다. 설계된 반사기에서 약 90%의 전반사를 위한 대역폭이 약 90%의 전투과를 위한 대역폭보다 매우 좁은 협대역 특성을 나타내었다.

• 전자공학회논문지A
• /
• 제33A권10호
• /
• pp.71-80
• /
• 1996

Sattering problem of electromagnetic waves by periodic strip grating with two dielectrics over a ground plane in case of oblique incidence and arbitrary polarization is analyzed by the vector floquet mode expansion method and the moment mehtod from the viewpoint of soft and hard boundary value problem. To confirm proposed analysis methods, we examine the solution convergence for the scattering problem. And some numerical results of artificially soft and hard surfaces using the structure filled with single dielectric slab between periodic strip grating and gorund plane is compared with previous results. Some interesting results for soft and hard surfaces using periodic strips loaded with two layered dielectric slabs over a ground plane are given.