• 제목/요약/키워드: Adiabatic model

검색결과 171건 처리시간 0.026초

CARS를 이용한 DOHC 스파크 점화 기관의 말단 가스 온도 측정 (End-Gas Temperature Measurments in a DOHC Spark-Ignition Engine Using CARS)

  • 최인용;전광민;박철웅;한재원
    • 한국자동차공학회논문집
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    • 제7권7호
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    • pp.122-128
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    • 1999
  • CARS(Coherent anti-Stokes Raman Spectroscopy) temperature measurement under engine-like condition was validated by measuring unburned gas temperatures of premixed propane-air flame in a constant volume combustion chamber. The measured temperatures were compared with predictions of 2 zone flame propagation model. End-gas temperatures were measured were measured by CARS technique in a conventional 4 cylinder DOHC spark-ignition engine fueled with PRF 80. Cylinder pressure was measured simultaneously with CARS signal and used as a parameter on fitting CARS spectrum to library of theoretical spectra. There was a good agreement between the measured temperature and adiabatic core temperature calculated from measured cylinder pressure. Significant heating by pre-flame reaction in the gas was observed in the late part of compression stroke.

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설계유량을 고려한 천음속 축류압축기 동익의 삼차원 형상최적설계 (Aerodynamic Design Optimization of A Transonic Axial Compressor Rotor with Readjustment of A Design Point)

  • 고우식;김광용;고성호
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.639-645
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    • 2003
  • Design optimization of a transonic compressor rotor (NASA rotor 37) using response surface method and three-dimensional Navier-Stokes analysis has been carried out in this work. Baldwin-Lomax turbulence model was used in the flow analysis. Two design variables were selected to optimize the stacking line of the blade, and mass flow was used as a design variable, as well, to obtain new design point at peak efficiency. Data points for response evaluations were selected by D-optimal design, and linear programming method was used for the optimization on the response surface. As a main result of the optimization, adiabatic efficiency was successfully improved, and new design mass flow that is appropriate to an improved blade was obtained. Also, it is found that the design process provides reliable design of a turbomachinery blade with reasonable computing time.

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154kV, 3GVA급 초전도 송전케이블의 개념설계 (Conceptual Design of 154kv, 3GVA Class Superconducting Power Cable)

  • 오봉환;조전욱;오상수;권영길;하동우;류강식;장종근;남궁도
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1995년도 하계학술대회 논문집 A
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    • pp.156-159
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    • 1995
  • A superconducting power cable is one of the promising ways for transmitting huge electric power efficiently in the future. We performed a conceptual design of 154kV, 3GVA class superconducting power cable. The AC loss of superconductor was estimated by using the Bean model. The cross sectional area of stabilizer was calculated under the adiabatic condition. In this paper, the results of the conceptual design of superconducting power cable is described.

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종횡비에 따른 태양열 집광흡수기의 열전달특성 (Heat Transfer Charaeteristic of Solar Concentration Absorber by the Aspect Ratio)

  • 이용훈;이중섭;배강열;정효민;정한식
    • 동력기계공학회지
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    • 제6권1호
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    • pp.43-49
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    • 2002
  • This paper showed the study on the heat transfer into space by the aspect ratio of solar concentration absorber, and the purpose of this study was to obtain the optimum aspect ratio and tilt angle. The boundary conditions of a numerical model are assumed as follows : (1) The heat source is located at the center of absorber. (2) The bottom wall is opened and adiabatic. (3) The top, right and left walls are cooled wall. The parameters for the study are the tilt angles and the aspect ratio. The velocity vectors and isotherms were dense at wall side and the heat source. The mean Nusselt number had a maximum value at Ar=1:1 and ${\theta}=0^{\circ}$ and showed a low value as the tilt angles were increased.

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Uncertainty Quantification of the Experimental Spectroscopic Factor from Transfer Reaction Models

  • Song, Young-Ho;Kim, Youngman
    • Journal of the Korean Physical Society
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    • 제73권9호
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    • pp.1247-1254
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    • 2018
  • We study the uncertainty stemming from different theoretical models in the spectroscopic factors extracted from experiments. We use three theoretical approaches, the distorted wave Born approximation (DWBA), the adiabatic distorted wave approximation (ADWA) and the continuum discretized coupled-channels method (CDCC), and analyze the $^{12}C(d,p)^{13}C$, $^{14}C(d,p)^{15}C$ reactions. We find that the uncertainty associated with the adopted theoretical models is less than 20%. We also investigate the contribution from the remnant term and observe that it gives less than 10% uncertainty. We finally make an attempt to explain the discrepancy in the spectroscopic factors of $^{17}C(\frac{3}{2}^+)$ between the ones extracted from experiments and from shell model calculations by analyzing the $^{16}C(d,p)^{17}C$ reaction.

INVESTIGATING THE PULSAR WIND NEBULA 3C 58 USING EMISSION MODELS

  • Kim, Seungjong;Park, Jaegeun;An, Hongjun
    • 천문학회지
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    • 제52권5호
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    • pp.173-180
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    • 2019
  • We present IR flux density measurements, models of the broadband SED, and results of SED modeling for the Pulsar Wind Nebula (PWN) 3C 58. We find that the Herschel flux density seems to be slightly lower than suggested by interpolation of previous measurements in nearby wavebands, implying that there may be multiple electron populations in 3C 58. We model the SED using a simple stationary one-zone and a more realistic time-evolving multi-zone scenario. The latter includes variations of flow properties in the PWN (injected energy, magnetic field, and bulk speed), radiative energy losses, adiabatic expansion, and diffusion, similar to previous PWN models. From the modeling, we find that a PWN age of 2900-5400 yrs is preferred and that there may be excess emission at ${\sim}10^{11}Hz$. The latter may imply multiple populations of electrons in the PWN.

Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting

  • Pagani, Alfonso;Carrer, Erasmo
    • Advances in aircraft and spacecraft science
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    • 제3권1호
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    • pp.77-93
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    • 2016
  • In this paper, a zero-dimensional mathematical formulation for rapid and explosive decompression analyses of pressurized aircraft is developed. Air flows between two compartments and between the damaged compartment and external ambient are modeled by assuming an adiabatic, reversible transformation. Both supercritical and subcritical decompressions are considered, and the attention focuses on intercompartment venting systems. In particular, passive and active vents are addressed, and mathematical models of both swinging and translational blowout panels are provided. A numerical procedure based on an explicit Euler integration scheme is also discussed for multi-compartment aircraft analysis. Various numerical solutions are presented, which highlight the importance of considering the opening dynamics of blowout panels. The comparisons with the results from the literature demonstrate the validity of the proposed methodology, which can be also applied, with no lack of accuracy, to the decompression analysis of spacecraft.

3D Radiation-Hydrodynimics for surface turbulence of Low-mass Stars

  • Bach, Kiehunn;Kim, Yong-Cheol
    • 천문학회보
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    • 제44권1호
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    • pp.84.3-84.3
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    • 2019
  • We investigate 3D radiation-hydrodynamics (RHD) for surface convection of the solar-type low-mass stars (M = 0.8, 0.9, and 1.0 Msun). The outer convection zone (CZ) of low-mass stars is an extremely turbulent region composed of partly ionized compressible gases at high temperature. Particularly, the super-adiabatic layer (SAL), the top of the CZ is the transition region where the transport of energy changes drastically from convection to radiation. In order to accurately describe physical processes, a realistic treatment of radiation should be considered as well as convection. As a starting model, the initial stratification in the outer envelope calculated using the solar calibrations in the context of the standard stellar theory. When the numerical fluid becomes thermally relaxed, the thermodynamic structure of the steady-state turbulent flow was explicitly collected. In this presentation, we compared thermodynamic properties of turbulent convection of the solar-type low-mass stars.

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Determination of the Kinetic Energy Release Originating from the Reverse Critical Energy in Unimolecular ion Dissociation

  • Yeh, In-Chul;Lee, Tae-Geol;Kim, Myung-Soo
    • Bulletin of the Korean Chemical Society
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    • 제15권3호
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    • pp.241-245
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    • 1994
  • A method has been developed to estimate the kinetic energy release originating from the reverse critical energy in unimolecular ion dissociation. Contribution from the excess energy was estimated by RRKM theory, the statistical adiabatic model and the modified phase space calculation. This was subtracted from the experimental kinetic energy release distribution (KERD) via deconvolution. The present method has been applied to the KERDs in $H_2$, loss from $C_6H_6^+$ and HF loss from ${CH_2CF_2}^+$. In the present formalism, not only the energy in the reaction coordinate but also the energy in some transitional vibrational degrees of freedom at the transition state is thought to contribute to the experimental kinetic energy release. Details of the methods for treating the transitional modes are found not to be critical to the final outcome. For a reaction with small excess energy and large reverse critical energy. KERD is shown to be mainly governed by the reverse critical energy.

2차원 및 3차원 정상상태 모델에 의한 수평브릿지만 결정성장에서의 고 - 액 계면과 편석 (Melt-solid interface and segregation in horizontal bridgman growth using 2 - and 3 - dimensional pseudo - steady - state model)

  • 민병수;김도현
    • 한국결정성장학회지
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    • 제5권4호
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    • pp.306-317
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    • 1995
  • 수평 브릿지만법은 갈륨 비소 반도체 결정을 성장시키는데 많이 사용된다. 수평 브릿지만 법에 의하여 성장된 단결정 내에서 불순물 분포를 알아보기 위하여 성장 과정 중의 액상에서 열전달, 물질전달, 유체흐름과 고상에서 열전달을 의사 정상상태를 가정하여 2차원 및 3차원 모델을 세우고 유한요소법에 의하여 수치모사하였다. 이때 고-액 계면의 위치와 형태도해의 일부분으로 다른 해들과 동시에 구하였다. 2차원 단열 경계조건에서는 3차원의 계면이 2차원의 경우보다 덜 휘어졌고, 대류 강도는 비슷하였다. 대류강도의 증가에 따라 수직 편석은 최대값을 보였으나 계면이 2차원에서 더 휘어져 최대값은 2차원에서 대류 강도가 더 작을 때 나타났다.

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