• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.127-131
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• 2006

An optimization algorithm is applied to a calibration task. In this paper, test data correlation, a reverse analysis method, is presented. With this method, flow rate and heat transfer rate, which are difficult to be measured are estimated using measured pressure and temperature data for helium pressurization system of launch vehicle.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.5
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• pp.1756-1762
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• 1991

본 연구에서는 막냉각되는 터빈블레이드에서의 열전달 계수를 측정하기 위하 여 열전달과 물질전달의 상사관계를 이용하였다.터빈블레이드의 선단을 다른 연구 에서와 마찬가지로 원봉으로 모사하였고, 원봉의 표면에 위치하고 있는 1열의 분사홀 로부터 제트가 분사될 때 분사홀 근처 및 그 하류에서의 물질 전달계수를 측정하기 위 해 나프탈렌승화법을 이용하였다. 분사홀 열의 위치를 정체점에서 하류방향으로 이 동시키면서, 물질전달계수의 변화를 연구하였고, 분사율(M=.rho.$_{j}$ U$_{j}$ /.rho.$_{\infty}$ U$_{\infty}$)의 영향도 고찰하였다.

• Journal of Energy Engineering
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• v.15 no.1 s.45
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• pp.35-44
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• 2006

This study experimentally investigates effect of boiling heat transfer when ultrasonic vibration was applied. Under the wall temperature condition, temperature distribution in a cavity was measured during the boiling process and heat transfer coefficient of convection, sub-tooled boiling and saturated boiling states were measured with and without ultrasonic vibration, respectively. Also, the profiles of the pressure distribution in acoustic field measured by a hydrophone were compared with the augmentation ratios of heat transfer calculated by local heat transfer coefficient. Result of this study, heat transfer coefficient and augmentation ratio of heat transfer is higher with ultrasonic waves than without one. Especially, augmentation ratio of heat transfer is more increased the convection state than sub-cooled boiling and saturated boiling states. Acoustic pressure is relatively higher near ultrasonic transducer than other points where is no installed it and affects the augmentation ratio of heat transfer.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.2
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• pp.72-79
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• 2003

A numerical calculation was conducted to estimate and to elucidate the role of the radiative heat flux from metal particles(Al, $Al_2O_3$) on the dynamic extinction of solid propellant rocket where the rapid depressurization took place. Anon-linear flame modeling implemented by the residence time modeling for metalized propellant was adopted to evaluate conductive heat flux to the propellant surface. The radiative heat feed back was calculated with the aid of a modified comvustion-flow model as well. The calculation results with the propellant of AP:Al:CTPB=76:10:14 had revealed that the radiative heat flux is approximately 5~6% of total flux at the critical depressurization rate regardless of chamber geometry (open or confined chamber). It was also found that the dynamic extinction in open geometry could be predicted at the depressurization rate about 45% larger with radiative heat feedback than without radiation. Thus, it should be claimed that even a small amount of radiative flux 5~6% could produce a big error in predicting the critical depressurization rate of the metalized propellant combustion.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2010.04a
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• pp.44-44
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• 2010

대부분의 산업분야에서 사용되는 공업로는 연소 시 $1000^{\circ}C$이상의 고온 배기가스가 배출되고 있기 때문에, 이들 배기가스로부터 폐열을 회수하여 에너지를 절감하고자 열교환기를 사용하고 있다. 하지만 현재 사용되고 있는 금속 소재의 열교환기의 경우 사용온도가 $800^{\circ}C$로 제한되어 있으며, 산화, 부식, creep등의 문제가 대두되고 있다. 본 연구에서는 세라믹 소재의 열교환기를 제작하여 열전달율, 공기누설율등을 평가하는 성능실험을 하였다. 실험방법은 연소시작 후 정상상태에 도달하기까지의 경향을 알아보고 공기유량과 가스유량에 변화를 주었을 때, 열전달율과 공기누설율등을 평가하고 이론적인 데이터와 비교하였다. 실험 결과, $1300^{\circ}C$이상의 환경에서도 정상적으로 작동하였으며, 외부환경조건을 고려하였을 때, 이론적인 데이터와 근접한 데이터를 얻을 수 있었다. 그러나 대류열전달에 의한 열손실과 공기누설등이 문제점으로 지적되었다. 향후 연구에서는 대류열전달에 의한 열손실을 고려한 연구와 효과적인 씰링으로 누설을 줄일 수 있는 실험장치를 개발할 필요가 있다.

• Journal of the KSME
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• v.18 no.4
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• pp.27-34
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• 1978

열에너지의 저장시스템은 축열채조, 열전달기기와 용기 및 보온재의 3개 주요부로 이루어진다. 축열재료는 현열계의 경우 온도가 상승하거나 잠열이용의 경우 상변화가 생기는 재료를 말한다. 열전달기기는 열에너지를 열원으로부터 축열재로 건열시키거나 축열재로부터 열부하측으로 열에 너지를 전달시키는 역할을 한다. 보온이 된 용기는 축열재를 외부로부터 열차단이 되도록 하여 외부로의 에너지 손실이 없도록한다. 열에너지저장시스템의 주성능득성은 용량, 에너지전달원, 저장온도에 의하여 주어진다. 여기서 용량은 축열재가 저장할 수 있는 에너지의 양을 뜻하고 열 전달율은 에너지원으로부터 축열재료로 또는 반대로 축열재료로부터 에너지부하측으로 전달시킬 수 있는율을 의미한다. 축열온도는 현열계에서는 축열재의 온도가 된다. 이 해설에서는 최근 발간 된 수 개의 자료를 발췌하여 간략히 그 내용을 알리고자 한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.4
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• pp.35-40
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• 2011

An experimental study of the flame response in a turbulent premixed combustor has been conducted in order to investigate mechanisms for combustion instabilities in a lean premixed gas turbine combustor. A lab-scale combustor and mixing section system were fabricated to measure the flame transfer function. Measurements are made of the velocity fluctuation in the nozzle using hot wire anemometry and of the heat release fluctuation in the combustor using chemiluminescence emission. The results show that the flame transfer functions are greatly dependent on the modulation frequency as well as operating conditions such as equivalence ratio. Flame dynamics can be generalized as a function of Strouhal number which is a ratio of flame length to modulation wave length.

• Journal of the Korean Society of Propulsion Engineers
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• v.2 no.2
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• pp.56-63
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• 1998

The present study investigated local heat transfer characteristics around a film cooling hole with variations of free stream turbulence intensity The film cooling jet is injected through a single hole inclined at $30^{\cire}$ to the surface and laterally at $45^{\cire}$ for the blowing rates of 0.5, 1.0 and 2.0. Turbulence generating grids are used at upstream of the film cooling hole to change the turbulence intensity of free stream. Free stream turbulence intensity without grids is 0.5%. Two different turbulence generating grid is installed at different at locations upstream of the film cooling hole so that turbulence intensity of free stream varies from 3% to 10%. The naphthalene sublimation technique has been employed to determine local heat/ mass transfer coefficients. With low free stream turbulence intensity, heat/mass transfer augmented area by coolant or free stream is distinguished evidently. However, when free stream turbulence intensity is high, heat transfer is enhanced in all region and heat transfer enhanced regions are not clearly divided due to vigorous mixing of coolant and free stream. The peak values of heat/mass coefficients are decreased and the distributions of heat/mass transfer coefficients are more uniform with high turbulence intensity. The effect of turbulence intensity on heat transfer characteristics is more evident as blowing rate is higher.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.6
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• pp.98-106
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• 2011

This paper reviews the state-of-the-art thermoacoustic(TA) modeling techniques and research trend to predict major parameters determining combustion instabilities in lean premixed gas turbine combustors. Linear TA modeling results give us an information on eigenfrequencies and initial growth rate of the instabilities. For the prediction, linear relation equation between acoustic waves and heat release oscillations should be derived in the determined system. Key information for this analysis is to determine the heat release fluctuations in the combustor, which is typically obtained by using n-${\tau}$ function from flame transfer function measurements and/or predictions. Great advancement in the linear TA modeling has been made over a couple of decades, and some successful prediction results have been reported in actual gas turbine combustors. However nonlinear TA model developments which are required to analyze nonlinear system behaviors such as limit cycle saturation and transition phenomena are still limited in a very simple system. In order to fully understand combustion instabilities in a complicated real system, nonlinear flame dynamics and acoustic wave interaction with nonlinear system boundary conditions should be explained from the nonlinear TA model developments.

• Proceedings of the Korean Society Of Semiconductor Equipment Technology
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• 2004.05a
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• pp.147-153
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• 2004

본 연구에서는 MOCVD 반응기의 온도분포가 필름 성장률에 미치는 영향에 대해 분석하였다. 온도해석에는 반응기 벽면의 전도열전달과 기체의 대류열전달이 포함되었다. 또 서셉터와 실험에 사용된 그래파이트 평판 사이의 웨이퍼 미세 간극을 해석에 포함하여 반응기 내부의 온도를 예측하였다. 정밀한 온도해석을 통해 얻은 반응기의 온도 분포를 이용하여 GaAs와 InP의 필름성장률을 해석하였으며 그 결과 미세 틈새가 GaAs의 필름 성장률에 영향을 미치는 것을 확인하였다.