• Title/Summary/Keyword: 입구조건

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Numerical calculation of Laminar flow in a Square Duct of 90° Bend (정사각형 단면을 갖는 90° 곡관의 층류유동 계산)

  • Kim H. T.;Kim J. J.
    • Journal of computational fluids engineering
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    • v.2 no.1
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    • pp.1-7
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    • 1997
  • A FA-FD hybrid method, developed for solving three-dimensional incompressible Navier-Stokes equations, is applied to calculate three-dimensional laminar flows through a square duct with a 90° bend. The method discretizes the convective terms in the primary flow direction with 3rd-order upwind finite-differences and the convective and diffusive terms in the transverse directions with the two-dimensional finite analytic method. The non-staggered grid system is used and the pressure-velocity coupling is achieved by a global iteration procedure based on the PISO algorithm. Detailed comparisons between the computed solutions and the available experimental data are given mainly for the velocity distributions at cross-sections in a 90° bend of a square duct with both fully developed and developing entry flows. Although the computational result shows generally a good agreement with the experimental data, there are some significant discrepancies underlining the necessity of more accurate numerical methods as well as reliable experimental data for their validation.

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Performance Analysis of Methanol Fueled Marine Solid Oxide Fuel Cell System (메탄올 연료형 SOFC 시스템의 성능 평가)

  • Kim, Myoung-Hwan;Kil, Byung-Lea;Lim, Tae-Woo;Kim, Jong-Su;Oh, Sae-Gin;Park, Sang-Kyun;Kim, Mann-Eung;Lee, Kyung-Jin;Oh, Jin-Suk
    • Journal of Advanced Marine Engineering and Technology
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    • v.34 no.4
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    • pp.448-454
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    • 2010
  • The strengthened regulations for atmospheric emissions from ships have caused a necessity of new, alternative power system in ships for the low pollutant emissions and the high energy efficiency. Recently, new kinds of propulsion power system such as fuel cell system, which use hydrogen as an energy source, have been sincerely considered. The purpose of this work is to predict the performance of methanol fueled SOFC system and to analyze the influence of operating temperature, current density, S/C, and $H_2$ utilization ratio.

Performance Improvement of Free Power Gas Turbine Type Gas Turbine Engine by Using of a MAT Cycle (MAT사이클을 이용한 분리축 가스터빈 엔진의 성능향상에 관한 연구)

  • 공창덕;김경두;기자영;최인수
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2001.04a
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    • pp.54-58
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    • 2001
  • In order to Improve the performance of a free power turbine type gas turbine engine by injecting the atomized water into a compressor inlet., a study on Moisture Air Turbine (MAT) cycle was proposed. Compressor work by air-water mixtures in phase change was theoretically considered, and it was found that the water evaporation might reduce the compressor work. Cycle model calculations predicted that power increments of 21.7%, 20.2% and 18.4% by 1.5% water to the air flow rate at the compressor intake with rotational shaft speeds of 1000, 1210, 1350 rps were obtained, and also thermal efficiency due to the reduction of compressor work was improved.

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Effects of a Bearing Strut on the Performance of an Inducer for Turbopumps (베어링 지지부가 터보펌프용 인듀서의 성능에 미치는 영향)

  • Choi, Chang-Ho;Noh, Jun-Gu;Kim, Jin-Sun;Hong, Soon-Sam;Kim, Jin-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.11
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    • pp.1022-1027
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    • 2007
  • Experimental and computational studies on a turbopump inducer with and without a bearing strut were performed to evaluate the effects of a strut on the performance of an inducer. Head rise, efficiency and surface static pressures were measured and compared with computational results. Generally a good agreement is observed between experimental and computational results, but some discrepancies are observed due to complex flow features such as backflows at the inlet and strut/inducer interactions. For the flow rates where the backflow region is large, installing a strut enhanced the hydraulic performance of the inducer by diminishing the size of the backflows. The results also show that the strut has negligible effect on the suction performance of the inducer.

Characterization of the internal flow and fuel spray from an impinging flow nozzle (노즐분공내 유체충돌이 있는 디젤노즐의 유동 및 분무특성 연구)

  • Ha, Seong-Eop;Kim, Heung-Yeol;Gu, Ja-Ye;Ryu, Gu-Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.12
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    • pp.1635-1646
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    • 1997
  • The nozzle length to diameter ratio of real diesel nozzles is about 2-8 which is not long enough for a fully developed and stabilized flow. The characteristics of the flow such as turbulence at the nozzle exit which affect the development of the spray can be enhanced by impinging the flow inside nozzle. The flow details inside the impinging nozzles have been investigated both experimentally and numerically. The mean velocities, the fluctuating velocities, and discharge coefficients in the impinging inlet nozzles, round inlet nozzle, and sharp inlet nozzle were obtained at various Reynolds number. The developing feature of the external spray were photographed by still camera and the droplet sizes and velocities were also measured by laser Doppler technique. The spray angle was greater and the droplet sizes near the spray axis were smaller with the impinging flow inside nozzle.

Experimental Study on Heat Transfer with Swirling Flow in a Cylindrical Annuli (원형동심관내 선회유동의 열전달에 대한 실험적 연구)

  • Chang, Tae-Hyun;Kil, Sang-Cheol;Lee, Kwon-Soo
    • Journal of the Korean Society of Visualization
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    • v.8 no.1
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    • pp.53-60
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    • 2010
  • Experimental investigations were conducted to study the characteristics of turbulent swirling flow in an axisymmetric annuli. Swirl angle measurements were performed using a flow visualization technique using smoke and dye liquid for Re=60,00080,000. Using the two-dimensional particle image velocimetry method, we found the time-mean velocity distribution and turbulent intensities in water with swirl for Re=20,000, 30,000, and 40,000 along longitudinal sections. Neutral points occurred for equal axial velocity at y/(R-r)=0.70.75, and the highest axial velocity was recorded near y/(R-r)=0.9. Negative axial velocity was observed near the convex tube along X/(D-d)=3~23. Another experimental study was performed to investigate heat transfer characteristics of turbulent swirling flow in an axisymmetric annuli. Static pressure, and local flow temperature were measured using tangential inlet condition and the friction factors and Nusselt number were calculated for several Reynolds numbers.

Experimental Investigation on Forced Convective Heat Transfer Characteristic Generated to Heated Tube (가열된 튜브에서 발생하는 강제 대류열전달 특성에 관한 실험적 연구)

  • Park, Hee-Ho;Lee, Yang-Suk;Kim, Sun-Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.3
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    • pp.90-98
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    • 2006
  • The Heated Tube Facility(HIF) was fabricated to identify the forced convective heat transfer and the cooling characteristic for the hydrocarbon fuel(Jet A-1), which is used for the coolant of the regenerative cooling system. The forced convective heat transfer coefficient was calculated from the measured coolant and tube surface temperature. In case of using the Jet A-1, the maximum heat flux which the coolant can absorb was identified by determining the critical wall temperature generating the burnout on the fixed flow condition. The inlet bulk-temperature of the coolant has a direct influence on the forced convective heat transfer characteristic.

Exergy Analysis of Regenerative Steam-Injection Gas Turbine Systems (증기분사 재생 가스터빈 시스템의 엑서지 해석)

  • Kim, Kyoung-Hoon;Jung, Young-Guan;Han, Chul-Ho
    • Journal of the Korean Society of Propulsion Engineers
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    • v.13 no.4
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    • pp.45-54
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    • 2009
  • An exergy analysis is carried out for the regenerative steam-injection gas turbine systems which has a potential of enhanced thermal efficiency and specific power. Using the analysis model in the view of the second law of thermodynamics, the effects of pressure ratio, steam injection ratio, ambient temperature and turbine inlet temperature are investigated on the performance of the system such as exergetic efficiency, heat recovery ratio of heat exchangers, exergy destruction, loss ratios, and on the optimal conditions for maximum exergy efficiency. The results of computation show that the regenerative steam-injection gas turbine system can make a notable enhancement of exergy efficiency and reduce irreversibilities of the system.

A Study on Effects of Large Tip Clearance in a Turbine Cascade (터빈캐스케이드에서 큰 팁간극에 의한 효과에 관한 연구)

  • Lee, Hyo-Seong;Song, Seung-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.33-36
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    • 2010
  • Lots of studies about turbine loss have been done especially about tip leakage loss. But these studies deals with small tip clearances which is less than 5 percent chord. Now, like turbopumps, small turbines have larger tip clearance and it is hardly found related papers in open literature. On this study, with varying tip clearance 1% to 20% chord, loss is measured under inlet velocity at 30m/s and Reynolds number based on chord at 210000. It is found that maximum loss coefficient is 0.113 at 10% clearance, and when tip clearance is larger than 10%, loss is not linearly increased anymore.

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Effect of air inflow on the performance of a 50kW-class cross-flow turbine (50kW급 횡류수차 내 공기 유입이 성능에 미치는 영향)

  • Kim, Jun-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.4
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    • pp.418-423
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    • 2014
  • Small hydropower has been considered as a solution to resolve the problem of exhaustion of fossil fuel and industrial pollution. In this study, we developed and tested a Cross-Flow Turbine with two guide vanes to optimize the small hydropower for the site condition with large fluctuation of head and flow rate. Furthermore, in the condition of constant inlet head, CFD analysis was carried out to analyze the effect of air suction and valve position on the performance characteristics. The results showed that the air suction can minimize the hydraulic loss caused by the Recirculation flow in the runner passage and flow impact on main shaft so that it can increase the turbine efficiency and output power.