• 제목/요약/키워드: stress wave speed

검색결과 72건 처리시간 0.031초

회전하는 구의 공력특성에 수치해석적 연구 (A Computational Study of Aerodynamic Characteristics of Spinning Sphere)

  • ;이영기;김희동
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.223-226
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    • 2006
  • Computational Study of a sphere subjected to free stream flow and simultaneously subjected to spinning motion is carried out. Three dimensional compressible Navier-Stokes equations are solved using fully implicit finite volume scheme. SST(Shear Stress Transport) $k-{\omega}$ turbulence model is used. Aerodynamic characteristics being affected are studied. Validation of the numerical process is done for the no spin condition. Variation of drag coefficient and shock wave strength with increase in spinning rate is reported. Changes in the wake region of the sphere with respect to spinning speed are also observed.

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실시간 홀로그래픽 간섭법을 이용한 유체의 가시화 (Visualization and Measurement of Fluids with Real-time Holographic Interferometry)

  • 엄철;강영준;김동우;유원재;안중근
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.539-544
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    • 2001
  • The holographic measurement techniques can be applied to various industrial fields such as automobile, airplane, construction, electronics, medical, mechanics and physics. The visualization of fluids is very important in aerodynamics, heat transfer and stress analysis. There are classically optical methods such as shadowgraph, schlieren method, and Mach-Zehnder interferometry for visualizing the fluid flow phenomena. But, it is difficult to understand the continuous state of fluids well in those methods. In this study, the real-time holographic interferometer with high-speed camera is applied to the flow visualization. In addition, collimated laser beam and rotating wedge are used for recording and formation of carrier fringes, respectively.

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Assessment of whipping and springing on a large container vessel

  • Barhoumi, Mondher;Storhaug, Gaute
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제6권2호
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    • pp.442-458
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    • 2014
  • Wave induced vibrations increase the fatigue and extreme loading, but this is normally neglected in design. The industry view on this is changing. Wave induced vibrations are often divided into springing and whipping, and their relative contribution to fatigue and extreme loading varies depending on ship design. When it comes to displacement vessels, the contribution from whipping on fatigue and extreme loading is particularly high for certain container vessels. A large modern design container vessel with high bow flare angle and high service speed has been considered. The container vessel was equipped with a hull monitoring system from a recognized supplier of HMON systems. The vessel has been operating between Asia and Europe for a few years and valuable data has been collected. Also model tests have been carried out of this vessel to investigate fatigue and extreme loading, but model tests are often limited to head seas. For the full scale measurements, the correlation between stress data and wind data has been investigated. The wave and vibration damage are shown versus heading and Beaufort strength to indicate general trends. The wind data has also been compared to North Atlantic design environment. Even though it has been shown that the encountered wind data has been much less severe than in North Atlantic, the extreme loading defined by IACS URS11 is significantly exceeded when whipping is included. If whipping may contribute to collapse, then proper seamanship may be useful in order to limit the extreme loading. The vibration damage is also observed to be high from head to beam seas, and even present in stern seas, but fatigue damage in general is low on this East Asia to Europe trade.

실내 온도가 뉴로에너지에 미치는 영향에 관한 연구 (A Study on the Indoor Temperature effects on Neuro-energy)

  • 김정민;김명호
    • 한국산학기술학회논문지
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    • 제15권4호
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    • pp.2436-2442
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    • 2014
  • 본 연구는 상대습도 50[RH%], 조도 1,000[Lux] 및 기류 속도 0.02[m/sec]의 동일한 조건의 항온 항습실에서 온도를 18, 23, 25, 28 및 $31[^{\circ}C]$로 변화를 주어 EEG, HRV 및 바이브라이미지를 비교 분석하였다. 실험 결과, 온도 $25[^{\circ}C]$에서 상대 $M{\alpha}$파, 상대 $M{\beta}$파, $\frac{SMR}{\theta}$ 및 SDNN은 활성화되었으며, ${\alpha}$파의 비대칭지수 $A_2$, HRT, 스트레스지수 및 피로도는 감소하였다. 따라서, 온도 $25[^{\circ}C]$가 쾌적성, 생산성 및 집중력 등과 같은 뉴로에너지 향상에 효과적인 것을 알 수 있었다.

다양한 하중 조건에서 Tetrapod 소파블록의 취약부 분석 (Evaluation of the Weak Part for Wave Dissipating Blocks under Various Conditions: Tetrapod)

  • 임정현;원덕희;한택희;강영종
    • 한국산학기술학회논문지
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    • 제15권8호
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    • pp.5385-5392
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    • 2014
  • 최근 전 지구적인 기상 변화로 인하여 슈퍼 태풍이 많이 발생되고 있다. 특히 2012년에는 볼라벤과 덴바 등 최대 풍속 60m/s 이상의 태풍이 우리나라에 상륙을 하였다. 설계 파고보다 높은 이상 고파랑이 내습하면서 소파블록을 포함한 항만시설물의 유실 및 파괴가 발생하였다. 우리나라는 주로 Tetrapod 블록이 가장 많이 설치되어 있음에도 불구하고 이에 대한 구조적 평가가 제대로 이루어지지 않았다. 이에 본 연구에서는 다양한 하중 조건하에서 Tetrapod 블록의 응력 메커니즘을 분석하고 취약부분을 분석하였다. 분석 결과 블록이 무근 콘크리트로 되어 있기 때문에 인장력에 가장 취약한 것으로 나타났으며, 4개의 다리가 연결되는 부분이 가장 취약하여 균열이 시작되는 것으로 분석되었다. 접합부를 부분 보강한다면 취약부가 감소될 것으로 판단된다.

지표층의 탄성계수 측정을 위한 새로운 탄성파 방법 (CHARACTERIZATION OF GEOTECHNICAL SITES BY MULTI-CHANNEL ANALSIS OF SURFACE WAVES(MCASW))

  • 박춘병
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 1995년도 가을 학술발표회 논문집
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    • pp.15.2-22
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    • 1995
  • Evaluating stiffness of near-surface materials has been one of the critically important tasks in many civil engineering works. It is the main goal of geotechnical characterization. The so-called deflection-response method evaluates the stiffness by measuring stress-strain behavior of the materials caused by static or dynamic load. This method, however, evaluates the overall stiffness and the stiffness variation with depth cannot be obtained. Furthermore, evaluation of a large-area geotechnical site by this method can be time-consuming, expensive, and damaging to many surface points of the site. Wave-propagation method, on the other hand, measures seismic velocities at different depths and stiffness profile (stiffness change with depth) can be obtained from the measured velocity data. The stiffness profile is often expressed by shear-wave (S-wave) velocity change with depth because S-wave velocity is proportional to the shear modulus. that is a direct indicator of stiffiiess. The crosshole and downhole method measures the seismic velocity by placing sources and receivers (geophones) at different depths in a borehole. Requirement of borehole installation makes this method also time-consuming, expensive, and damaging to the sites. Spectral-Analysis-of-Surface-Waves (SASW) method places both source and receivers at the surface, and records horizontally-propagating surface waves. Based upon the theory of surfacewave dispersion, the seismic velocities at different depths are calculated by analyzing the recorded surface-wave data. This method can be nondestructive to the sites. However, because only two receivers are used, the method requires multiple measurements with different field setups and, therefore, the method often becomes time-consuming and labor-intensive. Furthermore. the inclusion of noise wavefields cannot be handled properly, and this may cause the results by this method inaccurate. When multi-channel recording method is employed during the measurement of surface-waves, there are several benefits. First, usually single measurement is enough because multiple number (twelve or more) of receivers are used. Second, noise inclusion can be detected by coherency checking on the multi-channel data and handled properly so that it does not decrease the accuracy of the result. Third, various kinds of multi-channel processing techniques can be applied to f1lter unwanted noise wavefields and also to analyze the surface-wavefields more accurately and efficiently. In this way, the accuracy of the result by the method can be significantly improved. Fourth, the entire system of source, receivers, and recording-processing device can be tied into one unit, and the unit can be pulled by a small vehicle, making the survey speed very fast. In all these senses, multi-channel recording of surface waves is best suited for a routine method for geotechnical characterization in most of civil engineering works.

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수중충격하중을 받는 선체구조의 충격 및 파손 해석 (The Shock and Fracture Analysis of Ship Structure Subject to Underwater Shock Loading)

  • 정기태;김경수;김영복
    • 대한조선학회논문집
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    • 제32권1호
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    • pp.118-131
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    • 1995
  • 수중폭발을 받게 되는 해군 함정이나 충격하중을 받게 되는 초고속선의 구조에 대한 내충격 파손해석을 거시해석(global or macro analysis)과 미시해석(fine or micro analysis)의 두 단계로 나누어 수행하였다. 거시해석은 이중근사기법(DAA : Doubly Asymptotic Approximation)을 이용하였다. 심한 충격하중을 받는 구조는 주로 세 가지 파괴모드를 나타내는데 이는 충격후기에 주로 나타나는 동소성좌굴(Dynamic plastic buckling)에 기인하는 소성대변형과 충격초기에 주로 나타나는 인장 파괴(Tensile tearing failure)와 횡전단파괴(Transverse shear failure)가 있다. 본 논문의 미시해석에서는 잠수구조의 종보강재에 충격압력이 가해진 경우에 대하여 응력파(stress wave)의 파급과 이 응력파와 균열과의 상호작용에 의한 동적응력강도계수 $K_I(t)$의 계산함으로써 인장 파괴모드(Tensile tearing failure mode)해석을 수행하였다. 특히, 동적응력강도계수 $K_I(t)$의 계산에 있어서 실험적 방법으로 널리 사용되는 shadow optical method of caustic로부터 개발된 numerical caustic method를 사용하였다. 본 논문의 충격파손해석 수치 예로서 해석모델을 완전잠수주상체로 잡고 거시해석을 수행한 후 이로부터 구한 충격압력을 입력자료로 하여 종보강재에 대하여 미시해석을 수행하였다.

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The interaction between helium flow within supersonic boundary layer and oblique shock waves

  • Kwak, Sang-Hyun;Iwahori, Yoshiki;Igarashi, Sakie;Obata, Sigeo
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.75-78
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    • 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.

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초고압 $SF_6$ 가스차단기의 소전류 차단성능 해석기술 I (Evaluation Method I of the Small Current Breaking Performance for SF(sub)6-Blown High-Voltage Gas Circuit Breakers)

  • 송기동;이병운;박경엽;박정후
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제50권7호
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    • pp.331-337
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    • 2001
  • With the increasing reliability of analysis schemes and the dramatically increased calculating speed, the computer simulation has become and indispensable process to predict the interruption capacity of circuit breakers. Generally, circuit breakers have to possess both the small current and large current interruption abilities and the circuit breaker designers need to evaluate its capacities to save the time and the expense. The analysis of small current and the large current interruption performances have been considered separately because the phenomena occurring in a interrupter are quite different. To analyze the dielectric recovery after large current interruption many physical phenomena such as heat transfer, convection and arc radiation, the nozzle ablation, the ionization of high temperature SF(sub)6 gas, the electric and themagnetic forces and so forth mush be considered. However, in the analysis of small current interruption performance only the cold gas flow analysis needs to be carried out because the capacitive current is to small that the influence from the current can be neglected. In this paper, an empirical equation which is obtained from a series of tests to estimate the dielectric recovery strength has been applied to a real circuit breaker. The results of analysis have been compared with the test results and the reliability has been investigated.

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CFD를 이용한 고압파이프 파단 시 초음속제트의 압축성유동 특성에 관한 수치해석 (Numerical Analysis on the Compressible Flow Characteristics of Supersonic Jet Caused by High-Pressure Pipe Rupture Using CFD)

  • 정종길;김광추;윤준규
    • 대한기계학회논문집B
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    • 제41권10호
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    • pp.649-657
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    • 2017
  • 고압의 파이프 파단 시 파이프 내에 있던 유체가 고속으로 대기로 분출될 때 압축성유동을 동반하는 초음속제트가 발생한다. 이러한 초음속제트는 일반적으로 복잡한 비정상거동을 보여줄 수 있다. 본 연구는 이러한 고압파이프에서 분출되는 초음속제트에 의해 생성되는 압축성유동을 고찰하기 위하여 전산유체역학 해석이 수행되었다. 분출기체의 종류 및 파이프직경 변화에 따른 비정상유동 특성을 해석하기 위해 SST $k-{\omega}$ 난류모델이 채택되었다. 전산해석 시 기본 경계조건은 파이프직경 10 cm, 제트 압력비 5, 기체온도 300 K로 가정하였다. 그 해석결과로 초음속제트로 인해 생성되는 충격파의 거동이 관찰되었고, 간접적인 영향으로 폭풍파도 발생됨을 알 수 있었다. 기체의 분자량이 가장 작은 $H_2$의 압력파 특성은 안전영역까지의 거리가 가장 짧았으며, 분자량이 비슷한 $N_2$, 공기 및 $O_2$는 큰 차이가 없었다. 또한 파이프직경이 커져 제트에 의한 영향범위도 더욱 증대됨을 알 수 있었다.