• Title/Summary/Keyword: large- amplitude

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Preliminary Result from Rapid Cadence Photometric Monitoring of HBC722

  • Baek, Gi-Seon;Green, Joel D.;Pak, Soo-Jong;Lee, Jeong-Eun;Eon, Yi-Seulj;Park, Won-Kee;Choi, Chang-Su;Kang, Won-Seok;Im, Myung-Shin
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.113.2-113.2
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    • 2011
  • We observed a low-mass pre-main sequence star, HBC722 (also known as $LkH{\alpha}$ 188 G4), with Camera for QUasars in EArly uNiverse (CQUEAN) attached to 2.1 Otto Struve telescope at McDonald Observatory, USA. HBC722 is a new FU orionis-type object in the direction of NGC7000/IC5070, which produced large amplitude optical outbursts (${\delta}V$=4.7 mag over one year) for a few months and reached the peak in 2010 September. We carried out the photometric observation in SDSS r,i, and z band in 2011 April, July and August to monitor the long term decrease of its brightness. We also made continuous observation in r-band for half night in July, and whole two nights in August to investigate short term variability which could be related to the rotation of the central star or the inner circumstellar disk. In this poster, we present a preliminary result of the photometric observation for HBC722.

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Thermal diffusivity measurement of two-layer ar-coating systems using photoacoustic effects (광음향 효과를 이용한 2층 무반사 코팅막의 열확산도 측정)

  • 권경업;최문호;김석원;한성홍;김종태
    • Korean Journal of Optics and Photonics
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    • v.9 no.6
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    • pp.380-384
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    • 1998
  • As the development of ultrahigh power laser system, the laser mirrors must require high-resistant and effectively cooled. So, the study for the optical multilayer systems having large thermal diffusivity become important. In this study, we designed and fabricated two-layer anti-reflection (AR) optical coating samples, in different evaporation conditions of coating speeds (10, 20 $\AA$/s) and substrate temperatures (50, 100, 150, 20$0^{\circ}C$), using two dielectric materials $MgF_2$ and ZnS which have different refractive indices and measured the through-plane thermal diffusivity by using photoacoustic effect. The optical thicknesses of $MgF_2$ and ZnS layer were fixed as 5/4λ (λ=514.5nm) and λ, respectively, and the thermal diffusivity of the samples fabricated in the different conditions was obtained from the measured amplitude of photoacoustic signals by changing chopping frequency of $Ar^+$ layer beam. The results told us that the thermal diffusivity of the sample fabricated in the condition of 10 $\AA$/s and 15$0^{\circ}C$ showed the largest value.

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Numerical and experimental investigation of conventional and un-conventional preswirl duct for VLCC

  • Shin, Hyun-Joon;Lee, Jong-Seung;Lee, Kang-Hoon;Han, Myung-Ryun;Hur, Eui-Beom;Shin, Sung-Chul
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.5 no.3
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    • pp.414-430
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    • 2013
  • This paper shows the study of preswirl duct as an effective energy saving devices that have been devised and reviewed to support the propeller performance, especially for the ship of VLCC with large block coefficients. From the bare hull wake measurements, typical upper/lower asymmetry of hull wake at the propeller disk was found. The 2 kinds of pre-swirl duct, Unconventional half circular duct and Conventional circular pre-swirl duct have been designed and reviewed to recover the loss of propeller running in that condition. The general function of the pre-swirl duct was set to work against this asymmetry of wake and generate pre-swirled flow into the propeller against the propeller rotating direction. The optimum self propulsion tests with various angle configurations were carried out and the best configuration was decided. Accordingly, cavitation test was carried out with best configuration of unconventional half circular duct. The blade surface and tip vortex cavitation behaved smoother when the duct was mounted. The hull pressure amplitudes reflected this difference, so the hull pressure amplitude with duct was smaller than that of without duct.

Prediction of Failure for a Motor Stator by Monitoring Magnetic Flux Spectrum in High Frequency Region (고주파 영역 자속 스펙트럼 감시에 의한 전동기 고정자 고장예측)

  • Kim, Dae-Young;Yeo, Yeong-Koo;Lee, Jae-Heon
    • Plant Journal
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    • v.8 no.3
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    • pp.49-54
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    • 2012
  • In this study, the way how we can find the defects of motor windings in advance will be discussed. The magnetic flux spectrum in the high frequency region of the large motor was analyzed based on the actual fault practices related with motor windings. In case of defective motor relative amplitude ratio of the stator slot frequency to its sideband was very high compared to that of healthy motor. And the defective signal related with motor windings was indicated in advance in the magnetic flux spectrum prior to over 1 month before failure. Considering this aspect it can be estimated that magnetic flux spectrum in the high frequency region has the excellent predictive diagnostic capability.

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Effect of Tunnel Entrance Shape of High Speed Train on Aerodynamic Characteristics and Entry Compression Wave (고속전철의 터널입구 형상이 공력특성 및 터널입구 압축파에 미치는 영향)

  • Jeong, Soo-Jin;Kim, Woo-Seung;Zhu, Ming
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.6
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    • pp.111-118
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    • 2004
  • The work presented in this paper concerns the aerodynamic characteristics and compression wave generated in a tunnel when a high speed train enters it. A large number of solutions have been proposed to reduce the amplitude of the pressure gradient in tunnels and some of the most efficient solutions consist of (a) addition ofa blind hood, (b) addition of inclined part at the entrance, and (c) holes in the ceiling of the tunnel. These are numerically studied by using the three-dimensional unsteady compressible Euler equation solver with ALE, CFD code, based on FEM method. Computational results showed that the smaller inclined angle leads to the lower pressure gradient of compression wave front. This study indicated that the most efficient slant angle is in the range from $30^{\circ}$ to $50^{\circ}$. The maximum pressure gradient is reduced by $26.81\%$ for the inclined angle of $30^{\circ}$ as compared to vertical entry. Results also showed that maximum pressure gradient can be reduced by $15.94\%$ in blind hood entry as compared to $30^{\circ}$ inclined tunnel entry. Furthermore, the present analysis showed that inclined slant angle has little effect on aerodynamic drag. Comparison of the pressure gradient between the inclined tunnel hood and the vertical entry with air vent holes indicated that the optimum inclined tunnel hood is much more effective way in reducing pressure gradient and increasing the pressure rise time.

Analysis of Faceted-Reflector Antenna (각면 반사판 안테나의 해석)

  • Kwak, Chang-Soo;Uhm, Man-Seok;Yom, In-Bok
    • Journal of Satellite, Information and Communications
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    • v.5 no.2
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    • pp.34-39
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    • 2010
  • Due to big demand for satellite and communication service using personal handheld terminals, demand for satellites with huge antennas is increasing correspondingly. While such large antennas are realized by various types of deployable antennas, the reflecting surface is made by many facets irrespective of deploying mechanisms. In order to analyze the faceted-reflector more accurately, an existing ray-tracing method is improved. The algorithm allows the rays to cross each other, which is the main characteristic of the faceted-reflector, and takes unevenness of amplitude and phase over the aperture plane into consideration. For the study of the effect of facet configuration, facet generating algorithm is devised. From the analysis algorithm and the facet-generating algorithm, it has been found that the number of facets in a radial direction affects both directivity and sidelobe level. On the other hand, the number of facets in a circumferential direction affects sidelobe level only.

Behavior of Oil-Water Interface between Tandem Fences (이중 유벽 사이의 기름과 물의 계면의 거동)

  • Kang Kwan Hyoung;Lee Choung Mook
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.2 no.2
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    • pp.70-77
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    • 1999
  • The disturbance of oil-water interface confined between tandem fences caused by a sequence of traveling vortices below the interface is investigated. The traveling vortices are assumed to be those detached from the tip of the fore fence. The potential flow is assumed and the density interface is replaced as a sheet of vortex. The shape of the interface is predicted by tracing a finite number of marker particles placed at the interface. The velocity of the marker particles is determined by the Biot-Savart integral along the vortex sheet plus the contribution from the traveling point vortices. The rate of change of vortex-sheet strength is predicted by using an evolution equation for vorticity. The calculated results obtained for various conditions demonstrate that the large amplitude of interfacial wave following the moving vortek can be generated by the vortices.

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Nonlinear Prediction of Nonstationary Signals using Neural Networks (신경망을 이용한 비정적 신호의 비선형 예측)

  • Choi, Han-Go;Lee, Ho-Sub;Kim, Sang-Hee
    • Journal of the Korean Institute of Telematics and Electronics S
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    • v.35S no.10
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    • pp.166-174
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    • 1998
  • Neural networks, having highly nonlinear dynamics by virtue of the distributed nonlinearities and the learing ability, have the potential for the adaptive prediction of nonstationary signals. This paper describes the nonlinear prediction of these signals in two ways; using a nonlinear module and the cascade combination of nonlinear and linear modules. Fully-connected recurrent neural networks (RNNs) and a conventional tapped-delay-line (TDL) filter are used as the nonlinear and linear modules respectively. The dynamic behavior of the proposed predictors is demonstrated for chaotic time series adn speech signals. For the relative comparison of prediction performance, the proposed predictors are compared with a conventional ARMA linear prediction model. Experimental results show that the neural networks based adaptive predictor ourperforms the traditional linear scheme significantly. We also find that the cascade combination predictor is well suitable for the prediction of the time series which contain large variations of signal amplitude.

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A Strength Analysis of the Hull Gilder among the Rough Sea according to Ship Types (대파고 파랑중에서의 선체장도 해석에 관한 연주 - 선종에 따른 강도, 응답특성비교 -)

  • Sa-Soo Kim;Ku-Kyun Shin;Sung-Wan Son;Jae-Hong Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.30 no.4
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    • pp.153-168
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    • 1993
  • The ship sailing among waves suffers from the various wave loads that comes from its motion throughout its life. In the rationally-based design, the dynamic structural analysis is carried out using dynamic wave loads provided from the results of the ship motion calculation as the rigid body. This method is based on the linear theory assumed low wave height and small amplitude of motion. But at the rough sea condition, relatively high wave compared to the height ship's depth is induced the large ship motion, so configuration of the ship section below waterline changes rapidly at each time. This re-sults in a non-linear problem. Considering above situation we have already introduced the non-linear dynamic strength analysis method for the hull girder(refer vol. 29. No.4 November, 1992, Journal of SNAK). In this paper, estimation of the hull girder strength for various ship types such as tankers, containers and log carriers is carried out based on the introduced non-linear method. We expect that the results will be used as useful basic data for the es-timation of dynamic strength of ships in the rough sea.

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Effects of Oil Inlet Pressure and Temperature on the Dynamic Behaviors of a Full-Floating Ring Bearing Supported Turbocharger Rotor (터보차저 공급 오일 압력과 온도가 풀-플로팅 베어링의 동적 거동에 미치는 영향)

  • Lee, In-Beom;Hong, Seong-Ki
    • The KSFM Journal of Fluid Machinery
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    • v.20 no.2
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    • pp.53-62
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    • 2017
  • In this paper, the effect of oil conditions in rotor dynamic behaviors of a FFRB (Fully-Floating Ring Bearing) is investigated. Through the characteristic of a FFRB has two films, it has several advantages such as less friction loss and better stability over a wide speed range. However, it is difficult to supply a oil to the inner film. Thus, turbocharger makers have been paid significant attention to the lubrication of a FFRB because of its importance. This work focuses on the influence of oil inlet pressure and temperature. The methodologies of computational simulation and experimental test were used to estimate the rotor dynamic behaviors. In experimental test, the single-scroll turbocharger for the 1.4L diesel engine was used. The results show that the oil inlet pressure and temperature will place considerable influence on the rotor response. Oil conditions affect RSR (Ring Speed Ratio) which is cause of sub-synchronous vibrations, which also cause of oil whirling and whip even a critical speed. At higher speed range, the phenomenon of self-excited vibrations which is cause of instability of fluid whirl is investigated through the orbit shapes that consist of small orbit and large amplitude orbit. It is shown that some performance of a FFRB can be controlled by the conditions of oil supply. Finally, it was revealed that the oil induced operating conditions will strongly affect the turbocharger rotor dynamics behaviors.