• 수산해양기술연구
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• 제27권1호
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• pp.1-12
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• 1991

적분방식에 의한 어군량추정법을 실험적으로 검증하기 위하여, 실험수조에서 50 kHz와 200 kHz의 주파수를 대상으로 모의어군의 분포밀도와 초음파산란강도의 관계를 검토하고, 또 계량어군탐지기의 정도를 개선하기 위한 문제들에 대하여 고찰을 행한 결과를 요약하면 다음과 같다. 1. 어체의 모의표적으로 이용한 steel ball (직영 35mm)의 실측 echo 파형은 이론 echo 파형과 잘 일치하였다. 2. 5 종류의 주파수에 대하여 고등어 (체장 36cm)의 반사주파수특성을 조사한 결과, 측정주파수가 변화함에 따라 어체에 의한 echo 신호의 진폭과 파형이 크게 변동하고 있음을 알 수 있었다. 3. 송수파기의 음속 내에서 5개/m 상(3)와 30개/m 상(3)의 표적 군이 서로 상하로 존재할 때, 상부 표적군의 존재에 의해 하부 표적군의 echo level이 -0.43 dB 감쇠하는, 소위 그늘효과(shadowing effect)가 발생하였다. 4. 동지나해에서 정박 중에 탐지한 고밀도 어군의 echo신호와 그 어군직하의 해저에서 산란된 echo 신호를 상호 연관시켜 분석한 결과, 어군층내에서 발생한 어군감쇠와 다중산란효과가 해저 echo 신호의 변동에 큰 영향을 미치고 있음을 알 수 있었다. 5. 정치망의 원통에 인망한 정어리의 단위체적당에 대한 분포밀도가 36마리/m 상(3)였을 때, 해저기녹이 소실되는 어군감쇠현상과, 어군 echo 신호가 해저까지 신장되는 다중산란현상이 동시에 발생하였다. 6. 50kHz와 200kHz의 주파수에서 표적군의 평균체적산란강도(:dB)와 표적의 분포밀도($\rho$:개/m 상(3))의 간에 다음의 회귀직선식을 얻었다. 50kHz : =-46.2+13.7 Log($\rho$). 200kHz : =-43.9+13.4 Log($\rho$). 7. 표적의 분포밀도가 5, 10, 15, 20, 25, 30 개/m 상(3)였을 때, 적분방식에 의한 추정치는 50kHz에서 2.0, 8.1, 9.9, 14.1, 19.2, 26.7 개/m 상(3)이었고, 200kHz에서는 2.0, 8.0, 9.1, 15.0, 20.1, 24.1 개/m 상(3)이었으며, 단위체적당에 분포하는 표적의 수가 많을수록, 그 추정치의 정도가 높아지는 경향을 나타내었다. 또한, 양주파수에서 분포밀도의 추정치는 실제보다 약 30%정도 과소추정되었다.

• The Korean Journal of Physiology
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• 제21권2호
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• pp.259-272
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• 1987

This was study carried out to investigate the effect of calcium on spontaneous contraction and electrical activity induced by ethanol in gastric smooth muscle. After peeling off the mucous membrane from the isolated whole stomach of 102 cats, two kinds of small muscle preparations $(2.0{\times}0.2\;cm)$, one longitudinal and the other circular, were excised from the fundus, the corpus and the antrum portion of each whole stomach specimen. The isometric contraction of the small muscle preparation was measured in a cylinder-shaped chamber filled with Krebs-Ringer-dextrose solution (pH 7.4, temperature $36{\pm}0.5^{\circ}C$) bubbling with 5% $CO_2$ in $O_2$. A large muscle preparation $(5.0{\times}1.2\;cm)$ was excised from the anterior wall of the corpus-antrum portion of the same specimen in 72 of 102 cats. The gastric electrical activity (slow wave and spike potential) was monopolarly recorded by four capillary electrodes (Ag-AgCl), of which two were placed on the corpus and two on the antrum, in a muscle chamber filled with the same solution as described above. Changes in the amplitude of the contraction, frequency of the gastric slow wave and the production of the spike potential were observed after adding ethanol and/or under the treatments with verapamil, $CaCl_2$ and Ca-free Krebs-Ringer-dextrose solution. The results were as follows: 1) After adding ethanol, the spontaneous phasic contraction of the corpus was reduced dose-dependently (0.125-2.0%), which was totally abolished by higher concentrations (2.0-8.0%) of ethanol. 2) The corporal phasic contraction was also completely abolished by verapamil $(3{\times}10^{-5}\;M)$ or Ca-free Krebs-Ringer-dextrose solution. The contraction was increased by $CaCl_2\;(1.8{\times}10^{-3}\;M)$, but the inhibitory effect of ethanol on the contraction persisted even under the treatment with $CaCl_2$. 3) At higher concentrations, ethanol caused tonic contraction of both preparations from the fundus, the corpus and the antrum in a dose-dependent manner. The tonic contraction of the fundus produced by ethanol was not influenced by $CaCl_2$ or verapamil, whereas the tonic contraction was not produced by ethanol in tile Ca-free solution. 4) Frequency of gastric slow wave was decreased dose-dependently by the addition of ethanol (0.25-1.0%), and tile slow wave was not produced by higher concentration of ethanol (2.0%). 5) The frequency of slow wave was significantly reduced by verapamil only and the inhibitory influence of ethanol on the slow wave frequency was reinforced by verapamil. 6) The treatment of $CaCl_2$ increased significantly the slow wave frequency, and attenuated the inhibitory effect of ethanol on the frequency. It is therefore suggested that ethanol regulates the phasic contraction and the production of slow wave by interfering with the transport of calcium in the stomach muscle of the cat.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.91-93
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• 2003

A comprehensive numerical study is carried out to investigate for the understanding of the flow evolution and flame development in a supersonic combustor with normal injection of ncumally injecting hydrogen in airsupersonic flows. The formulation treats the complete conservation equations of mass, momentum, energy, and species concentration for a multi-component chemically reacting system. For the numerical simulation of supersonic combustion, multi-species Navier-Stokes equations and detailed chemistry of H2-Air is considered. It also accommodates a finite-rate chemical kinetics mechanism of hydrogen-air combustion GRI-Mech. 2.11[1], which consists of nine species and twenty-five reaction steps. Turbulence closure is achieved by means of a k-two-equation model (2). The governing equations are spatially discretized using a finite-volume approach, and temporally integrated by means of a second-order accurate implicit scheme (3-5).The supersonic combustor consists of a flat channel of 10 cm height and a fuel-injection slit of 0.1 cm width located at 10 cm downstream of the inlet. A cavity of 5 cm height and 20 cm width is installed at 15 cm downstream of the injection slit. A total of 936160 grids are used for the main-combustor flow passage, and 159161 grids for the cavity. The grids are clustered in the flow direction near the fuel injector and cavity, as well as in the vertical direction near the bottom wall. The no-slip and adiabatic conditions are assumed throughout the entire wall boundary. As a specific example, the inflow Mach number is assumed to be 3, and the temperature and pressure are 600 K and 0.1 MPa, respectively. Gaseous hydrogen at a temperature of 151.5 K is injected normal to the wall from a choked injector.A series of calculations were carried out by varying the fuel injection pressure from 0.5 to 1.5MPa. This amounts to changing the fuel mass flow rate or the overall equivalence ratio for different operating regimes. Figure 1 shows the instantaneous temperature fields in the supersonic combustor at four different conditions. The dark blue region represents the hot burned gases. At the fuel injection pressure of 0.5 MPa, the flame is stably anchored, but the flow field exhibits a high-amplitude oscillation. At the fuel injection pressure of 1.0 MPa, the Mach reflection occurs ahead of the injector. The interaction between the incoming air and the injection flow becomes much more complex, and the fuel/air mixing is strongly enhanced. The Mach reflection oscillates and results in a strong fluctuation in the combustor wall pressure. At the fuel injection pressure of 1.5MPa, the flow inside the combustor becomes nearly choked and the Mach reflection is displaced forward. The leading shock wave moves slowly toward the inlet, and eventually causes the combustor-upstart due to the thermal choking. The cavity appears to play a secondary role in driving the flow unsteadiness, in spite of its influence on the fuel/air mixing and flame evolution. Further investigation is necessary on this issue. The present study features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous works. In particular, the oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is not related to the cavity, but rather to the intrinsic unsteadiness in the flowfield, as also shown experimentally by Ben-Yakar et al. [6], The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The work appears to be the first of its kind in the numerical study of combustion oscillations in a supersonic combustor, although a similar phenomenon was previously reported experimentally. A more comprehensive discussion will be given in the final paper presented at the colloquium.

• 지질공학
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• 제31권4호
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• pp.603-620
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• 2021

수진기들을 서로 케이블로 연결하지 않고 독립적으로 운용하는 육상-노달 탄성파 기술을 수륙 경계지역에 대한 탄성파 반사법자료를 얻기 위해 사용하였다. 이 기술은 수진기 설치와 수거가 간편하기 때문에 지형조건 영향을 적게 받으면서 양호한 자료를 얻을 수 있다는 점에서 매우 경제적이다. 경상북도 포항시 형산강 하구를 테스트 지역으로 한 이 연구에서는 송수신 측선을 약 120 m 간격으로 서로 평행하도록 전개하여 음원은 강에서 에어건을 사용하고 무선 수신은 하상에 설치한 노달 시스템을 사용하였다. 수집된 반사파 자료들은 낮은 신호대잡음(S/N)과 불연속적인 이벤트를 보이며, 특히 직접파, 가이드파, 음파, Scholte 표면파를 포함한 대부분의 이벤트들이 현장 자료에서 쌍곡선 형태로 나타는데 이러한 특징은 송수신이 같은 측선에서 이루어지는 일반적인 탐사에서의 직선 형태와 크게 대비된다. 주된 자료처리는 저주파 고진폭 잡음에 가려진 미약한 신호를 향상시키기 위한 띠통과 필터링, 공기파를 완화시키기 위한 주파수-파수 필터링, 송수신기 사이의 전파시간을 보정하기 위한 시간지연 보정을 수행하여 궁극적으로 가이드파와 공기파에 가려진 천부의 반사파를 표출하는데 목적을 두었다. 송신기와 수신기 사이의 횡단-오프셋 거리에 따른 시간지연 보정을 위한 주시방정식과 곡선을 이 연구에서 새로이 제시하였다. 시간지연 보정 효과는 최소 횡단-오프셋 자료에서 보정 후 약 200 ms 상향 이동하는 잘 정렬된 수평층으로 잘 관찰된다, 직접파/공기파를 기준으로 한 시간지연 보정은 서로 평행한 송수신 측선에서 얻어지는 자료처리에 필수적인 것으로 나타났다. 이 연구에서 개발되고 적용된 육상 노달-수상 에어건 시스템 자료의 수집과 처리 기법은 차후 천부가스, 단층대, 연안지역 및 도심지의 엔지니어링 설계를 위해 육해상 경계 지역에서 얻어지는 고분해능 자료에 효과적으로 쉽게 적용될 것으로 기대된다.