• Title/Summary/Keyword: Cavity length

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A Study on the Stabilization Scheme of Optical Source for Precision Measurement (정밀측정을 위한 안정된 광원에 관한 연구)

  • 김지대;서호성;이동주
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2003.04a
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    • pp.265-271
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    • 2003
  • This study is for the stable optical source in order to get the precision measurement, which contributes to help the laser frequency and the output to be settled. The laser optical frequency is changed by the length of resonance cavity. The length variation of the laser resonance amplitude is affected by the thermal expansion of that system. So, we try not only to adjust the temperature of the laser tube using the heater for fine length of resonance cavity, but also to maintain the fixed temperature of the resonance cavity for outputting the safe laser optical frequency. Therefore, we must take materials with the thermal expansion of the supporting system, which is closer to it of the laser resonance cavity. Using the materials, we can promote to stabilize the temperature of it. In advance, we also plan to get the settlement of the laser frequency and the output in the long km, optimizing and stabilizing the system.

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Effect of Evacuation Variables on Pressure Change in the Die Cavity (다이캐스팅 금형 공간 내의 감압도에 미치는 제 변수의 영향)

  • Kim, Ki-Young
    • Journal of Korea Foundry Society
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    • v.20 no.3
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    • pp.181-187
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    • 2000
  • There are two types of vacuum die casting, one is known as the chill block method, and the other is the valve block method. Efficiency of the valve block method is better than the chill block method. However purchasing and maintaining cost of the former one is very high, the latter method is popular in many small and medium die casting shops. Simple evacuation system using chill vent was prepared to investigate the effect of the air pressure, hose length and chill vent type on the pressure change in die cavity in this study. The rate of evacuation was influenced by the evacuation method, chill vent condition and hose length. Evacuation time became longer and vacuum level lower when evacuating cavity via chill vent. It took a longer time to evacuate the cavity when a longer hose was used. Vacuum level in the cavity also decreased with increase in hose length.

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Characteristics of Flame-holding in a Scramjet Combustor with a Cavity

  • Tanaka, Hideyasu;Takahashi, Shuhei;Uriuda, Yoshitaka;Wakai, Kazunori;Tsue, Mitsuhiro;Kono, Michitaka;Ujll, Yasushige
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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    • pp.55-61
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    • 2004
  • Numerical simulations were conducted in a rectangular scramjet combustor with a cavity and/or a step in order to investigate their performances for flame-holding. Flow structures and OH radical profiles in the cavity and the step were calculated. The calculated results showed that the cavity generated a larger recirculation zone than the step that had the same depth. Additionally, the combustor with a cavity could make a large low-velocity area than the combustor with a step. The cavity performance was determined by its depth and length. The cavities with too large or too short length did not work effectively, and a certain aspect ratio showed high performance for flame-holding. There was a minimal depth under which the cavity did not work as flame-holder. The fuel injections upstream the cavity and inside the cavity were also tested to investigate the effects on the cavity performance. The result showed that the fuel injection inside the cavity reduced reaction areas and residence time. Therefore, the upstream injection was preferable to the inside injection.

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CAVITY OF CREATION FOR COLD FUSION AND GENERATION OF HEAT

  • Oh, Hung-Kuk
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1996.10b
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    • pp.3-12
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    • 1996
  • Cold fusion technologies now are being developed very successfully. The $\pi$-far infrared rays are generated from three dimensional crystallizing $\pi$-bondings of oxygen atoms in water molecules. The growing cavity in water molecules make near resonance state and a vortex of infrared rays and attracts $\pi$-far infrared rays in the water. The cavity surrounded by a lot of $\pi$-far infrared rays has a very strong gravitational field. The $\pi$-far infrared rays are contracted into $\pi$-far infrared rays of half wave length and of one wave length. The $\pi$-far infrared rays of half wave length generate heat while $\pi$-far infrared rays of one wave length are contracted into $\pi$-gamma rays of one wave length. The contracted $\pi$-gamma rays of one wave length make nucleons and mesons, which is the creation and transmutation of matter by covalent bondings and three-dimensional crystallizing $\pi$-bondings into implosion bonding. Patterson power cell generates a very strong gravitational cavity because the electrolysized oxygen atoms make $\pi$-far infrared rays than in plain water.

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The Study on Cavity Flow in Supersonic flow field (초음속 유동장에 놓인 공동 유동에 대한 연구)

  • Yoon Y. H.;Hong S. K.;Kwon K. B.
    • 한국전산유체공학회:학술대회논문집
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    • 2003.08a
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    • pp.139-143
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    • 2003
  • In this study the numerical analyses on cavity flow in supersonic flow field are conducted. According to the length-to-depth ratio of cavity, the shear layer is changed, consequently influencing on vortex structure inside the cavity. Especially in case the fluid flow outside cavity impinges inside the cavity, the oscillation of the cavity flow is identified. Another result is that though the cavity flow shows the unsteadiness, characteristics of cavity flow can be represented by pressure coefficients converged.

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Study of the unsteady pressure oscillations induced by rectangular cavities in a supersonic flow field

  • Krishnan L.;Ramakrishna M.;Rajan S.C.
    • 한국전산유체공학회:학술대회논문집
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    • 2003.10a
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    • pp.294-298
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    • 2003
  • The complex, unsteady, self-sustained pressure oscillations induced by supersonic flow past a rectangular cavity is investigated using numerical simulations. The present numerical study is performed using a parallel, multiblock solver for the two-dimensional, compressible Navier­Stokes equations. Open cavities with length-to-depth (L / D) ratio in the range 0.5 - 3.3 are considered. This paper sheds light on the cavity physics, cavity oscillatory mechanism, and the organisation of vortical structures inside the cavity. The vortex shedding phenomenon, the shear layer impingement event at the aft wall and the movement of the acoustic/compression wave within the cavity are well predicted. The vortical structures· and the source of the acoustic disturbances are found to be located near the aft wall of the cavity. With the increase in the cavity length, strong recompression of the flow near the aft wall leading to a sudden jump in the cavity form drag is observed. The estimated cavity tones are in good agreement with the available semi­empirical relation. Multiple peaks are noticed in deep and long cavities. For the present free­stream Mach number 1.71, it is observed that around L/D=2.0, the cavity oscillatory mechanism changes from the transverse to longitudinal oscillatory mode. The effects of this transition on various fluid dynamics and acoustic properties are also discussed.

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Cavity as a New Passive Device for Reduction of Skin Friction and Heat Transfer (새로운 수동제어소자인 공동을 이용한 마찰력과 열전달 감소에 관한 연구)

  • Hahn Seonghyeon;Choi Haecheon
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.463-466
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    • 2002
  • In order to examine the possibility of using a cavity as a passive device for reduction of skin friction and heat transfer, an intensive parametric study over a broad range of the cavity depth and length at different Reynolds numbers is performed for both laminar and turbulent boundary layers in the present study. Direct and large eddy simulation techniques are used for turbulent boundary layers at low and moderate Reynolds numbers, respectively. for both laminar and turbulent boundary layers over a cavity, a flow oscillation occurs due to the shear layer instability when the cavity depth and length are sufficiently large and it plays an important role in the determination of drag and heat-transfer increase or decrease. For a cavity sufficiently small to suppress the flow oscillation, both the total drag and heat transfer are reduced. Therefore, the applicability of a cavity as a passive device for reduction of drag and heat transfer is fully confirmed in the present study. Scaling based on the wall shear rate of the incoming boundary layer is also proposed and it is found to be valid in steady flow over a cavity.

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A Reexamination of the Method of Measuring Internal Loss and Quantum Efficiency in Laser Diodes (레이저 다이오드의 내부손실 및 내부 양자효율 측정법에 대한 재고찰)

  • 한영수;도만희;김상배;정상구
    • Journal of the Korean Institute of Telematics and Electronics A
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    • v.31A no.5
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    • pp.121-125
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    • 1994
  • We examine the conventional method of measuring the internal optical loss using the dependence of the reciprocal external quantum efficiency on the cavity length in laser diodes. It is shown that the implicit assumption of constant internal differential quantum efficiency ${\eta}_{id}$, which has been customarily misinterpreted as internal quantum efficiency ${\eta}_{i}$, is not valid for devices with short cavity length. Therefore, for reliable measurments long cavity data should be used.

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Numerical Analysis of Supersonic Combustion Flows according to Fuel Injection Positions near the Cavity (공동주위 분사위치에 따른 초음속 연소 유동해석)

  • Jeong Eunju;Jeung In-Seuck
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.368-373
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    • 2005
  • To achieve efficient combustion within a manageable length, a successful fuel injection scheme must provide rapid mixing between the fuel and airstreams. The aim of the present numerical research is to investigate the mixing enhancement combustion phenomena according to fuel injector location near the cavity in supersonic flow. Fuel injector location changes the actual length to depth ratio of the cavity in the supersonic combustor. Therefore fuel injector location near the cavity effects different fuel/air mixing efficiency and combustion efficiency.

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Heat Transfer in an Axisymmetric Cavity of a Rectangular Tube (사각관로의 축대칭 공동부에서의 열전달)

  • Park, Yong-Il
    • Solar Energy
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    • v.10 no.1
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    • pp.31-37
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    • 1990
  • An experimental study for the flow in an axisymmetric cavity of rectangular tube was performed. The pressure and heat transfer coefficient along the side and opposite-walls of the cavity were measured. The cavity length was varied from 80mm to infinity during the experiment. As the result of this study, it was found that as the length of cavity increased beyond the reattachment point, the heat transfer coefficient decreased. It was also found that the mean heat transfer coefficient became maximum near the reattachment point.

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