• Smart Structures and Systems
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• 제23권1호
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• pp.71-79
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• 2019

In general, it may be advantageous to measure the pressure pulsation near a valve to detect a valve defect in a linear compressor. However, the acceleration signals are more advantageous for rapid classification in a mass-production line. This paper deals with the performance improvement of fault classification using only the compressor-shell acceleration signal based on the relation between the refrigerant pressure pulsation and the shell acceleration of the compressor. A transfer function was estimated experimentally to take into account the signal noise ratio between the pressure pulsation of the refrigerant in the suction pipe and the shell acceleration. The shell acceleration signal of the compressor was modified using this transfer function to improve the defect classification performance. The defect classification of the modified signal was evaluated in the acceleration signal in the frequency domain using Fisher's discriminant ratio (FDR). The defect classification method was validated by experimental data. By using the method presented, the classification of valve defects can be performed rapidly and efficiently during mass production.

• 한국항공우주학회지
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• 제36권3호
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• pp.264-270
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• 2008

하이브리드 로켓 고체 연료의 연소율(Burning Rate)을 묘사하는 후퇴율은 연료 유속, 산화제 유속과 더불어 연료길이의 함수로 나타내어지나 일반적으로 가장 영향이 큰 산화제 유속만의 함수로 모델링된다. 그러나 이는 연료가 갖고 있는 고유의 열화학적 특성에 대한 영향이 내포되어 있지 않아 다양한 연료에 대한 공통된 관계를 나타내기 어렵다. 본 연구에서는 고체연료의 열화학적 특성과 연소에 따른 공기역학적 특성이 고려된 물질전달수(B Number)를 도입하여 다양한 연료에 공통으로 사용될 수 있는 연소율 관계식을 제시하고, 물질전달수 내의 공기역학적 특성의 영향을 분석하였다. 물질전달수와 산화제 유속의 함수로 표현된 연소율 식은 고정된 실험 지수항과 상수항으로 PMMA, PP 및 PE의 연소율을 모두 묘사할 수 있었고, 연소율 관계식에서 B Number에 내포된 공기역학적 효과는 미미하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.368-372
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• 2005

단일 포트 하이브리드 로켓의 다양한 연료에 따른 후퇴율 변화를 수행하였다. 연료는 PE, PMMA를 사용하였고, 산화제는 기체 산소를 사용하였다. 후퇴율은 산화제 유량뿐만 아니라, 연료의 열역학적 특성과도 관계가 있다. 본 연구에서는 물질 전달계수(B number)와 산화제 유량과의 관계를 고려한 실험식을 구하였다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2010년도 한국우주과학회보 제19권1호
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• pp.32.3-32.3
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• 2010

We have analyzed times of minima for six eclipsing binary systems which show asymmetric light curves. We found that five binary systems show period decrease and one system shows cyclic period variation. Three asymmetric light curves (SV Cen, RT Scl and VW Boo) are due to hot spot caused by mass transfer. Other three asymmetric light curves (AD Phe,, EZ Hya and TY Boo) are due to cool spot on the cooler component caused by magnetic activities. We also obtain absolute dimensions from photometric solution and spectroscopic solution by analyzing their light curves and radial velocity curves, collected from literatures, using 2007 version Wilson and Devinney computer code.

• 태양에너지
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• 제6권1호
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• pp.31-36
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• 1986

In this paper heat transfer characteristics in air-solid packed bed with spherical steel particles are studied experimentally. The effect of particle sizes (${\phi}1.5,\;{\phi}2.5,\;{\phi}3.96,\;{\phi}4.75,\;{\phi}5.95,\;{\phi}7.15$), bed sizes (${\phi}50,\;{\phi}60,\;{\phi}70,\;{\phi}80$) and mass flow rate are investigated. Also heat transfer effect of the bed with particles and without particles is compared in terms of heat transfer coefficient. As a result of this experiments, the following relation is obtained in the range of the Reynolds numbers 40 between 1500. $Nu= 0.8755\;Re^{0.6367}$ (40

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1996년도 춘계학술발표회논문집(2)
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• pp.227-232
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• 1996

The one-third calibrating relation by steady solution can cause large error when applied to an unsteady flow with large amplitude waves. Extended calibrating method, which can treat the normal convective contribution, is developed. The normal mass convective term is included into the 2-D mass transport equation by means of rms value and random function. The unknown shear rate is numerically determined by solving the 2-D mass transport equation inversely. This recovery method which predicts the unknown shear rate is constructed. It is found that it works very well without distortion. The inclusion of the normal convective term has a negligible effect on the mass transfer coefficient.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2005년도 동계학술발표대회 논문집
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• pp.591-596
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• 2005

The objectives in the present study are to investigate that the enhancement heat transfer was experimentally measured and was compared with the acoustic pressure obtained by numerical analysis. From the results of the present study, a strong Fluid motion initiated by ultrasonic vibrations can affect heat and mass transfer. This phenomenon. called acoustic streaming, clearly observed by PIV measurement leads to increase in velocity of a Fluid which is a crucial physical concept to explain the enhancement heat transfer. The heat transfer coefficient is increased with increase in the ultrasonic intensities. The largest enhancement heat transfer (about 26%) is measured at the ultrasonic intensity of 300W. Acoustic streaming results from sudden acoustic pressure variations in the liquid. The results of numerical analysis reveal that acoustic pressure is increased by 59.5% at the ultrasonic intensity of 300W. The higher acoustic pressure near four ultrasonic transducers develops more intensive flow destroying the flow instability. Also, the profiles of acoustic pressure variation are consistent with those of enhancement heat transfer.

• 설비공학논문집
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• 제11권2호
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• pp.250-261
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• 1999

Based on a set of performance plots relating the design variables to the imposed conditions, an easy-to-use and versatile design procedure for chevron-type multipass plate heat exchangers is developed. In order for the present procedure to cover multipass with unequal passes and non-unity ratio of heat capacity rate, each stream number of transfer unit is adopted as the basic design variable instead of the exchanger number of transfer unit. It is found that there exists a unique relation between the stream and exchanger number of transfer units regardless of the chevron angle and the plate length. In addition, for a given value of the pressure drop the heat transfer area per unit mass flow rate can be expressed in terms of the stream number of transfer unit only. These two relationships in the form of simple plots constitute the framework of design. The sample results in comparison with the available data indicate that the present procedure includes the previous ones as a subset, and that every design method is affected essentially by the selection of specific correlations for the heat transfer coefficient and the friction factor.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.223-227
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• 2006

하이브리드 추진 시스템에서의 산화제 종류에 따른 연소특성을 알아보기 위한 연구를 수행하였다. 산화제는 $GN_2O$와 GOX를 사용하고, 고체연료는 폴리에틸렌(PE)을 사용해 연소시험을 하였다. 산화제 종류에 따른 연소특성은 O/F 비에 따른 화염온도로 해석이 가능하였으며, $GN_2O$가 GOX보다 하이브리드 추진 시스템의 산화제로 효율이 좋음을 확인하였다 산화제의 유량은 직경이 다른 여러 개의 쵸킹 오리피스로 제어했고, 산화제 공급 유량범위는 $0.0138{\sim}0.0427kg/sec$ 이었다. 산화제 종류에 따른 연소특성을 표현하는 실험식은 고체연료의 질량유속으로 나타냈고, 이는 물질전달 수와 산화제의 질량유속으로 얻어진다.

• Journal of Mechanical Science and Technology
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• 제17권12호
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• pp.2087-2098
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• 2003

The development of numerical mathematical model to calculate both the static and dynamic characteristics of a multi-shaft gas turbine consisting of a single combustion chamber, including advanced cycle components such as intercooler and regenerator is presented in this paper. The numerical mathematical model is based on the simplified assumptions that quasi-static characteristic of turbo-machine and injector is used, total pressure loss and heat transfer relation for static calculation neglecting fuel transport time delay can be employed. The supercharger power has a cubical relation to its rotating velocity. The accuracy of each calculation is confirmed by monitoring mass and energy balances with comparative calculations for different time steps of integration. The features of the studied gas turbine scheme are the starting device with compressed air volumes and injector's supercharging the air directly ahead of the combustion chamber.