• 제목/요약/키워드: Flux-flow

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막냉각량 및 작동점 변화가 액체로켓 칼로리미터의 열유속에 미치는 영향 (Parametric Study on Heat Flux Characteristics of a Sub-scale Calorimeter)

  • 김종규;이광진;서성현;한영민;최환석;조원국
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제25회 추계학술대회논문집
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    • pp.346-350
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    • 2005
  • 연소압 50bar 이상의 연소조건에서 반복 사용이 가능하도록 제작된 물냉각형 칼로리미터에서 막냉각량 및 작동점의 변화 시 열유속의 특성을 알아보았다. 분사기 헤드와 칼로리미터 사이에 12개의 오리피스를 갖는 막냉각 링이 삽입된다. 칼로리미터는 연소실부와 노즐부로 구성되어 있으며, 총 19개의 냉각 채널로 구성되어 있다. 설계점 연소시험 시 막냉각량이 주 연료의 10.5% 유량일 때, 막냉각량이 없는 경우보다 노즐목에서의 최대 열유속은 약 30% 감소되었고, 막냉각량이 없는 경우, 탈설계점(OD3)이 설계점에 비해 노즐목에서의 최대 열유속이 약 31% 증가 하였다.

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Flow Field Analysis on the Stagnation Streamline of a Blunt Body

  • Lee, Chang-Ho
    • International Journal of Aeronautical and Space Sciences
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    • 제17권2호
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    • pp.149-156
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    • 2016
  • The hypersonic flow on the stagnation streamline of a blunt body is analyzed with quasi one-dimensional (1-D) Navier-Stokes equations approximated by adopting the local similarity to the two-dimensional (2-D)/axisymmetric Navier-Stokes equations. The governing equations are solved using the implicit finite volume method. The computational domain is confined from the stagnation point to the shock wave, and the shock fitting method is used to find the shock position. We propose a boundary condition at the shock, which employs the shock wave angle in the vicinity of the stagnation streamline using the shock shape correlation. As a result of numerical computation conducted for the hypersonic flow over a sphere, the proposed boundary condition is shown to improve the accuracy of the prediction of the shock standoff distance. The quasi 1-D Navier-Stokes code is efficient in computing time and is reliable for the flow analysis along the stagnation streamline and the prediction of heat flux at the stagnation point in the hypersonic blunt body flow.

전해수를 이용한 견섬유 정련 및 세리신 회수(II)-분리막에 의한 세리신 농축을 중심으로- (The Degumming and Sericin Recovery of the Silk fabric Using the Electrolytic Water(II))

  • 배기서;이태상;노덕길;홍영기
    • 한국염색가공학회지
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    • 제16권4호
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    • pp.10-18
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    • 2004
  • In this work, Aqueous sericin solution was prepared by degumming process with electrolytic reduction water. Then, the microfiltration and ultrafiltration systems were applied to the concentration of aqueous sericin solution. The objective of this study was to select the optimum operating condition among the different pressure. The permeate flux and rejection ratio were observed with time, pressure, flow rate and concentration. and, the wastewater and permeated water quality values such as pH, BOD, COD, and NH levels were measured. In order to see the influence of electrolytic reduction water, the flux of pure water and electrolytic reduction water by PVDF22(MF) and PS100(UF) membrane was measured. In microfiltration system, the relative flux reduction decreased rapidly to 0.02 in the 30min, as the concentration polarization and gel layer formation were increased. and then the sericin concentration rejection ratio was 40%. In ultrafiltration system, the permeate flux decreased with time and concentration, and increased with the operating pressure and flow rate. Optimal condition in PS100 membrane system for sericin concentration was operating pressure 1.464kgf/$cm^24, operating flow rate $7\ell/min at\; 40^{\circ}C$. At that time, sericin concentration rejection ratio was 83% respectably. The sericin solution was concentrated from 0.1wt% solution to 0.2 wt % solution during about 2 hrs by the UF filteration membrane system.

GOx/PC 하이브리드 로켓의 추력제어 환경에서 후퇴거리 예측 (Estimation of Propellant Consumption during Thrust Control of GOx/PC Hybrid Rocket)

  • 강완규;허환일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.526-529
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    • 2009
  • 본 연구에서는 Lab-Scale의 하이브리드 연소기를 이용하여 하이브리드 로켓의 추력제어 범위와 연소 시간에 따른 추진제의 후퇴거리를 분석하기 위하여 산화제 유량에 따른 추진제별 연소 특성을 파악하였다. 산화제 유량을 제어하기 위해서 니들 밸브와 스텝모터를 결합하여 스텝모터의 구동에 의해 니들밸브의 개폐량을 조절할 수 있도록 배관 시스템을 설계하였다. 산화제 유량 변화를 통해 추진제에 따른 질유량과 후퇴율 관계식을 유도하였다. 추력제어를 하면서 명령 추력 값에 따른 산화제 유량을 통해 후퇴거리를 예측하였으며 실제 추력제어 연소 실험을 통해 신뢰성을 확인하였다.

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이중 동심관 유동에서 핵비등 시발점의 영향인자에 대한 실험적 연구 (An experimental study on the effect of parameters for onset of nucleate boiling in concentric annuli flows)

  • 송주한;김경천;이승홍;박주환;석호천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.373-378
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    • 2000
  • An experimental investigation on the incipience of nucleate boiling in forced flow of water is performed as a verification and extension of previous analysis. The effects of the subcooling, Reynolds number and surface curvature on the onset of nucleate boiling(ONB) in a concentric annulus flow channel with smooth inner heating surface is investigated experimentaly. Through flow visualization, the boiling phenomenon was observed directly and the experimental results were examined to find ONB heat flux. The results show that the variation of heat flux at ONB is increased linearly as the Reynolds number and subcooling are increased. The effect of surface curvature is very great specially for a small radius when radius of the inner heating tube is increased, the heat flux at ONB is almost inversely increased for the range of this investigation. It is found that the effect of convex surface curvature on ONB heat flux is very significant for a small radius.

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경계요소법에 의한 파동장에 있어서 비선형파의 가상경계처리 (Open Boundary Treatment of Nonlinear Waves in the Shallow Water Region by Boundary Element Method)

  • 김남형;;최한규
    • 한국해안해양공학회지
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    • 제3권3호
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    • pp.176-183
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    • 1991
  • 본 연구는 경계요소법을 이용하여 비선형 자유표면파을 해석한 것이며, 가상경계처리는 유체 연속성을 고려하여 mass-flux와 energy-flux를 사용하여 유한진폭파동의 해석수법을 제시했다. 유체의 비선형성 때문에 증분법을 적용했으며 경계요소법에 의해 얻어진 결과는 유한요소법의 결과와 실험치와 비교하여 보았으며 좋은 일치가 얻어 졌다. 따라서, 이 방법은 광범위한 파동문제 해석에 유효하게 이용될 수 있으리라 사료된다.

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아음속 횡단류에 수직 분사되는 분무의 액적크기 및 속도 분포 특성 (Droplet Sizes and Velocities from Single-Hole Nozzle in Transversing Subsonic Air-stream)

  • 이인철;조우진;이봉수;김종현;구자예
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.106-109
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    • 2007
  • The spray plume characteristics of liquid water jet injected into subsonic cross-flow at 42 m/s were experimentally investigated. Nozzle has a 1.0 m diameter and L/D=5. Droplet sizes, velocities, volume flux were measured at each downstream area of the injector exit using phase Doppler particle anemometry. Measuring probe position is moved with 3-way transversing machine. Experimental results indicate that SMD is varied from 75 to $120{\mu}m$ distribution and it is uncertain layer structure. SMD peaks at the top of the spray plume. This phenomenon is related to the momentum exchange between column waves and cross-flow stream. Droplet vector velocities were varied from 11.5 to 33 m/s. A higher-velocity region can be identified in down edge region at Z/D : 40, 70 and 100. Lower-velocity region were observed on bottom position of the spray plume. Volume flux is a criterion to the droplet concentration. All volume flux distribution has a same structure that continuously decreases from the center region to the edge of the plume. Z/D : 20 is spatially less concentrated than in Z/D : 100.

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R-410A 비등열전달에 미치는 미세관경 0.5mm와 3.0mm의 영향 (Flow Boiling Heat Transfer of R-410A in 0.5mm & 3.0mm Diameter Horizontal Tube)

  • ;최광일;오종택
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.154-159
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    • 2008
  • Two-phase flow boiling heat transfer of R-410A in horizontal small tubes was reported in the present experimental study. The local heat transfer coefficients were obtained over a heat flux range of 5 to 40 kW/$m^2$, a mass flux range of 170 to 600 kg/$m^2s$, a saturation temperature range of 3 to $10^{\circ}C$, and quality up to 1.0. The test section was made of stainless steel tubes with inner diameters of 0.5 and 3.0 mm, and lengths of 330 and 3000 mm, respectively. The section was heated uniformly by applying a direct electric current to the tubes. The effects on heat transfer of mass flux, heat flux, inner tube diameter, and saturation temperature were presented. The experimental heat transfer coefficient is compared with six existing heat transfer coefficient correlations. A new boiling heat transfer coefficient correlation based on the superposition model for R-410A in small tubes was developed with mean deviation of 10.13%.

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수직 이착륙기의 고온 고속 배기열에 의한 함정 갑판의 열유속 계산을 위한 수치모델 (Numerical Estimation of Heat flux on the Deck Exposed to the High Temperature Impinging Jet of VTOL Vehicle)

  • 장호상;황세윤;최원준;이장현
    • 한국군사과학기술학회지
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    • 제21권1호
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    • pp.74-85
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    • 2018
  • This study has analyzed the convective heat transfer on the deck exposed to the high-temperature impingement exhausting from a VTOL vehicle. The heat flow of the impingement on the deck is modeled by the convection heat transfer. The convective heat flux generated by the hot impinging jet is investigated by using both convective heat transfer formulation and conjugate heat transfer formulation. Computational fluid dynamics(CFD) code was used to compute the heat flux distribution. The RANS equation and the k-e turbulence model were used to analyze the thermal flow of the impinging jet. The heat flux distribution near the stagnation zone obtained by the conjugate heat transfer analysis shows more reasonable than the convective heat transfer analysis.

Improvement of the critical heat flux correlation in a thermal-hydraulic system code for a downward-flow narrow rectangular channel

  • Wisudhaputra, Adnan;Yun, Byong Jo;Jeong, Jae Jun
    • Nuclear Engineering and Technology
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    • 제54권10호
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    • pp.3962-3973
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    • 2022
  • Several critical heat flux (CHF) correlations including the look-up table in the MARS code have been assessed for the prediction of CHF in a downward-flow narrow rectangular channel. For the assessment, we built an experiment database that covers pressures between 1.01 and 39.0 bar, gap sizes between 1.09 and 6.53 mm, mass fluxes up to 25,772 kg/m2s, and under one-sided and two-sided heating conditions. The results of the assessment showed that the Kaminaga correlation has the best overall prediction compared to others. However, because the correlation uses global variables, such as inlet and outlet subcooling and total heat transfer area, it is difficult to use in a system code. A new CHF correlation is then proposed by replacing the global variables in the Kaminaga correlation with local ones and adding correction factors to consider the effect of gap size, mass flux, and the number of heating walls. Additional correction factor is added to consider the effect of inlet subcooling. It is shown that the new one is better than the Kaminaga correlation and it is easy to implement to any system code.