• 한국분무공학회지
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• 제29권1호
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• pp.23-31
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• 2024

This study conducted a 3D thermo-acoustic analysis based on the helmholtz solver to analyze the major resonance modes causing combustion instability in a single-can combustor. The experimental investigations were carried out on a test rig designed by the Korea Institute of Machinery & Materials (KIMM) under various conditions of hydrogen co-firing and fuel staging. Through these experiments, two primary unstable frequencies were identified. To determine the resonance modes of these frequencies, a 3D thermo-acoustic analysis was conducted using temperature information from the test rig. The results confirmed that the unstable frequencies observed in the experiments were all longitudinal modes. Additionally, the mode shapes identified in the analysis facilitated a simplification of the exit geometry for the low-order network model, confirming that this did not significantly affect the fundamental resonance modes.

• 대한기계학회논문집
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• 제18권2호
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• pp.456-466
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• 1994

Experimental investigation was made to study the mechanism of fluid and thermal oscillation phenomena of surface-tension driven flow in a cylindrical liquid column heated from above which is the low-gravity floating zone simulated on earth. Hexadecane, octadecane, silicon oil (10cs), FC-40 and water are used as the test liquids. The onset of the oscillatory thermocapillary convection appears when Marangoni number exceeds its criteria value and is found to be due to the coupling among velocity and temperature field with the free surface deformation. The frequency of temperature oscillation decreases with increasing aspect ratio for a given diameter and Marangoni number and the oscillation level increases with Marangoni number. The flow pattern in the liquid column appears either as symmetric or asymmetric 3-D flow due to the oscillatory flow in the azimuthal direction. The free surface deformation also occurs either as symmetric or asymmetric mode and its frequency is consistent with those of flow and temperature oscillations. The amplitude of surface deformation also increases with Marangoni number.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.178.2-178.2
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• 2005

• 통합자연과학논문집
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• 제1권2호
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• pp.89-114
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• 2008

Interrelationship between heavy rainfalls and related with low-level jets(LLJ) is analyzed by using fifty cases of heavy rainfall events occurred over the Korean peninsula from 1992 to 2001. Those cases are classified with four synoptical features. There are 32% chances that the low pressure exist in heavy rainfall over than 150 mm per day case by case. Secondly Changma front and front zone account for 28% of all cases. The ratio of marine tropical boundary type and trough type record 22% and 18% respectively. The moist and warm south-westerly winds associated with low-level jets have been induced convective instability and baroclinic instability. Therefore, heavy rainfall due to the approach of a low pressure occurred at September and before Changma. During the period of Changma, this type has been happened heavy rainfall when low pressure and stationary front has vibrated south and north. Changma type has longer the duration time of precipitation than other types. Third type, located with marine Tropical boundary, have mainly rained in August and September. The last trough case locally downpoured in short time with developing cell. The occurrence low-level jets related to heavy rainfall has increased over 12.5 m/s wind speed. The result is that 43 heavy rainfalls out of 50 cases reach peak at the time of maximum precipitation intensity. Also, the variation of wet number and K-index corresponded with the variation of wind speed. It is found that the number of frequency of low-level jets with southwestward direction has been increased and these jets are mainly passed from the southwest toward to the northeast of the Korean peninsula in that time.

• 대한기계학회논문집B
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• 제22권4호
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• pp.450-467
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• 1998

The characteristics of the unstable impinging circular jet is investigated based on the frequency characteristics and the sound field of the impinging-tones. Two symmetric modes S1 and S2, associated with low frequency and high frequency respectively, and one helical mode H have been observed. At low speed the S2 mode is dominant and switched by the S1 mode as the speed increases. When the jet speed is high the S1 mode is very active over the impinging distance from half the nozzle diameter to its ten times, while the S2 mode occurs at shorter distance corresponding to stage 2 and 3. The helical mode H seems unstable, likely to be influenced much by the experimental environment, and occurs at relatively high speed with almost the same frequency characteristics as the S2 mode. By estimating the convection speed of the unstable jet, it is found that the ratio of the convection speed to the jet speed decreases with both Strouhal number and Reynolds number and the speed of S2 mode is faster than the Si mode. When the present experimental results are compared with the previous investigations performed for the hole tone and the impinging tone with a small plate, the S1 mode is found to be associated with the ring vortex of large diameter with low speed, but the S2 mode with the vortex of small diameter with high speed. In addition, the frequency is found to be influenced by the nozzle configuration but the characteristics is almost the same. From the impinging distance and frequency range, it can be deduced that S1 mode is related with the jet column mode and S2 mode with the shear mode.

• 한국추진공학회지
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• 제14권5호
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• pp.92-100
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• 2010

75톤급 기술검증용 연소기의 연소안정성 시험이 저압 조건에서 수행되었다. 이 시험에 사용된 두 개의 연소기 헤드 중 하나는 631개의 분사기를 가지며, 다른 하나는 721개의 분사기를 가진다. 631개의 분사기를 갖는 연소기 헤드는 연소압력 30 bar에서 자발 불안정이 발생하였고 721개의 분사기를 갖는 연소기 헤드는 동일한 연소압력과 동일한 유량 조건에서 고주파 연소안정성이 유지됨을 보였다. 그러나 721개의 분사기를 갖는 연소기 헤드는 연소압력 20 bar에서 자발 불안정이 발생하였고 이러한 결과로부터 연소기 헤드의 형상은 안정성 경계 영역을 변화시킴을 알 수 있었다.

• 제어로봇시스템학회논문지
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• 제13권11호
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• pp.1053-1059
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• 2007

This paper presents a target sate estimator(TSE) with low pass filter for improving the gun driving command. The ballistic computer uses target information such as predicted range, velocity, acceleration of a target to generate the gun command. We adopt the finite impulse response(FIR) filter as our TSE to shorten calculation time for the driving command and due to its inherent stability property. We also introduce a post-processing filter to reduce the high frequency components in the output signal of a TSE which may cause instability of gun driving. The first order low pass filter has been designed based on $H{\infty}$ criteria considering the noise characteristics. To show the validity of the present scheme, simulation results are given for the overall gun driving system including aircraft target information.

• 한국추진공학회지
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• 제18권6호
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• pp.19-26
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• 2014

70 N급 하이드라진 추력기 개발모델의 압력 불안정 특성 고찰을 위한 지상연소시험을 수행하였다. 단일추진제급 하이드라진이 연소시험용 추진제로 선정되었고, 촉매대에는 $Ir/Al_2O_3$ 촉매를 충전하였다. 추력실 직경변화가 연소안정성에 미치는 영향을 규명하기 위해 길이직경비(L/D) 1.03, 1.13, 1.26을 갖는 하단 추력실을 시험변수로 적용한 성능평가가 수행되었다. 개발모델은 50 Hz 근처의 저주파 불안정 특성을 내재하고 있으며, L/D 증가 및 작동압력의 감소가 정체실의 압력진동을 증대시킨다는 사실이 확인되었다.

• 전력전자학회논문지
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• 제15권1호
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• pp.43-51
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• 2010

본 논문에서는 고전압 전동기 가변속 장치인 H-브릿지 멀티레벨(H-Bridge Multi-Level; HBML) 인버터를 이용한 유도 전동기 벡터 제어시 인버터의 출력 전압 위상 지연 현상을 해석하고 전류 제어기의 보상 기법을 제시하였다. Phase-Shifted Pulse Width Modulation (PSPWM) 기법을 적용한 HBML 인버터는 개별 인버터 모듈이 독립적으로 동작할 수 있어서 확장성과 모듈화 능력이 향상되는 장점이 있다. 그러나 이러한 PSPWM을 적용한 HBML 인버터는 기준 전압과 실제 전압 사이에 위상 차이가 있기 때문에 출력 주파수에 대한 샘플링 주파수의 비율이 충분하지 않은 고속 영역에서 전류 제어기를 불안정하게 하는 원인이 된다. 전류 제어기의 불안정성은 기준 전압과 출력 전압의 위상 차이를 보상하는 제안된 방법을 추가함으로써 제거하였다. 본 방법은 인버터의 스위칭 주파수가 낮고, 전동기 속도가 높은 조건에서 PSPWM을 이용한 HBML 인버터 시스템에 효과적이며, 13레벨로 구성된 HBML 인버터로 구동되는 6,600[V] 1,400[kW] 유도전동기 실험을 통해 제안된 방법의 타당성을 입증하였다.

• Journal of Microbiology and Biotechnology
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• 제27권9호
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• pp.1711-1715
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• 2017

In this study, we characterized the $bla_{NDM-5}$-bearing plasmid in a Klebsiella pneumoniae isolate that had lost the plasmid during serial passage. We determined the complete sequences of the plasmid pCC1410-2, which was extracted from a K. pneumoniae ST709 isolate collected at a Korean hospital from which two NDM-5-producing K. pneumoniae isolates were subsequently isolated. As a result, the pCC1410-2 plasmid had a backbone structure that was similar to those of two plasmids previously reported from the same hospital, but lacked some antibiotic resistance genes ($bla_{TEM-1}$, rmtB, mphR(A), mrx(A), and mph(A)). A 9-bp repeating unit encoding three amino acids (Gln-Gln-Pro) was inserted in TraD in pCC1410-2. Thus, the pCC1410-2 plasmid might be transferred from the previously identified carbapenem-resistant K. pneumoniae, but some delections and inversions might have occurred during the process. We compared the transfer frequency and stability of the plasmids. The relative frequency of conjugative transfer and stability in the host were significantly lower in pCC1410-2 than in previously reported $bla_{NDM-5}$-bearing plasmids in Korea. A low transfer frequency and instability in the host may cause underestimation of carbapenemase-producing Enterobacteriaceae in the clinical setting and in surveillance studies.