• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.5
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• pp.71-78
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• 2002

Experiments have been performed using two-color PIV in hydrogen non-premixed flames with various conditions of coaxial air, which was classified into three cases with/without reaction. Mean velocity, turbulence intensity and Reynolds stress were analyzed using flow fields from PIV measurement First, the similarity of pure jet had a good agreement with previous results of other researchers. It was found that the decay of centerline velocity was proportional to $x^{-1}$ in coaxial air conditions. By normalizing axial distance with effective jet diameter defined by effective density, the data of centerline velocity collapsed a single line. And the radial profiles of mean velocity showed that they didn't become self-similar because the curves differed from each other as coaxial air velocity increased at fixed fuel velocity. Also, turbulence intensity became self-similar further downstream than mean velocity.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.4
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• pp.1-7
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• 2003

습공기에 포함된 수증기가 상(Phase)변화를 일으킬 때 잠열이 발생하고 이 잠열은 익형 주위의 압축성 유동 상태량들을 변화시키므로, 이러한 열 증가가 유동에 끼치는 영향에 대하여 수치해석을 통하여 연구 수행하였다. 수치해석은 Rusak 과 Lee [1]가 최근에 연구 수행한 미교란 방법(small-disturbance approach)에 근거하여 이루어졌다. 고전적 핵 생성 모델과 작은 물방울 성장(droplet growth)모델을 이용한 이 방법에서는 비평형 균질 응축과정에서 일어나는 열 방출을 묘사한다. 응축에 의한 열전달, 압축성 유동의 운동에너지, 그리고 유동의 열적 상태량들 사이에서 일어나는 비선형 상호영향을 조사하고, 또한 주어진 문제를 지배가호 있는 상사 파라미터들을 제시하였다. 계산 결과들은 Euler 방정식을 사용하여 얻은 선행 수치계산들과 비교하여 잘 일치됨을 보였다. 상사법칙은 유동 동역학과 응축 상태량들이 상당히 비슷하게 거동하는 다양한 유동 형태들을 제안한다. 압축성 습공기 유동은 유체기계에 사용되는 익형들의 공력 성능을 증가시키는데 응용될 수 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.561-565
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• 2009

The performance of supersonic impulse turbine was investigated experimentally. Experiment was performed with the compressed air instead of the high temperature burned gas because of the limitation of test facility and danger. As a result of the experiment with the compressed air, the performance in the real gas(burned gas) was predicted by the similarity method. The nozzle area of prototype turbine was calculated based on the real gas. So, it is difficult to satisfy the similarity conditions completely. Two similarity conditions were set and the design point for real gas was existed between two similarity conditions. And, the new turbine test model with calculated nozzle area based on the compressed air was tested. Therefore, similarity point of the new turbine test model was also existed between above two similarity points. It means that the design point for real gas was similar to the test point with the new turbine model.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.2
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• pp.39-45
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• 2006

In liquid rocket engine turbopump, it is difficult to evaluate turbine performance for high pressure, high temperature circumstance. Turbine test is often done by using air at similarity condition so that the turbine can be tested at lower risk. This paper describes an air similarity test program of liquid rocket engine turbopump turbine. A test facility has been built to evaluate aerodynamic performance of turbines. The test facility consists of high pressure air supply system, mass flow rate measuring nozzle, test section, hydraulic break, exit orifice for pressure control, instrumentation and control system. This paper also presents how to decide the similarity conditions of the turbine test and describes how to control test conditions. Relative standard deviation of measurement parameter was less than 1% and measured turbine efficiency corresponded with analysis result within 2%.

• The Journal of the Korea Contents Association
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• v.15 no.12
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• pp.572-585
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• 2015

The present study conducted in two parts toward employees in government office and state-owned companies, and financial companies. First, main impacts were demonstrated in the links between superior communication ability (SCA) and outcome variables (self-efficacy, and learning goal orientation). Second, mediating effects of self-efficacy and LGO were investigated in the relation SCA-Innovative behavior. The data which applied in analysis was collected from 318 employees who work at government office and state-owned companies, and financial companies in Jeju island. The results were as follows. First, SCA were positively associated with self-efficacy and LGO. Second, self-efficacy and LGO were fully mediated both relationships between SCA and innovative behavior. Findings were as follows. SCA is an important factor on self-efficacy and LGO. Such the results have meaningful implications in the research area of communication. The importance of self-efficacy and LGO were demonstrated when considering the both variable in the relations SCA-innovative behavior.

• 유체기계공업학회:학술대회논문집
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• 2003.12a
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• pp.73-79
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• 2003

The steam turbine efficiency is an important factor in power plant. Accurate evaluation of steam turbine performance is essential. However, it is not easy to evaluate the steam turbine performance due to its high temperature and high pressure circumstance. Therefore most steam turbine performance tests were conducted by air similarity test. This paper described a test program for air similarity test of steam turbine at Korea Aerospace Research Institute. A test facility has been designed and built to evaluate aerodynamic performance of turbines. The test facility consists of air supply system, single stage test section, power absorption system, instrumentation and auxiliary system. For evaluation of steam turbine performance, the test of single stage axial turbine air similarity performance was conducted and uncertainty analysis was performed.

• Proceedings of the Korea Water Resources Association Conference
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• 2020.06a
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• pp.150-150
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• 2020

본 연구에서는 수리모형실험을 통하여 원형 다단 실린더 게이트 형식의 취수시설에서 발생하는 공기연행을 분석하였다. 수리모형실험의 원형은 경상북도 청도군에 위치한 운문댐의 "운문댐 안전성 강화사업"에서 계획되고 있는 신설취수탑을 기준으로 상사법칙은 Froude상사법칙을 적용하고 1/20의 모형 축척을 가지는 취수탑의 국부모형에 하류단 수위를 고려하기 위해 유량조절시설을 설치하여 실험을 실시하였다. 실험조건은 크게 두 가지로 구분하였으며, 수면으로부터 유입구 상단부까지의 거리 ∆h1(m)과 유입부 저수지 저류 수위와 하류단 유량조절시설간의 수위차인 ∆h2(m)이며, ∆h1에 대한 조건은 0.01m~0.06m로 0.01m 간격으로 6가지, ∆h2에 대한 조건은 0.10m~1.70m로 0.20m간격으로 9가지로 이를 조합하여 총 54개 CASE에 대해 진행하였다. 실험결과 공기연행 발생 시 그에 따른 영향을 평가하기 위해 발생 정도에 따라 미발생(Not Occur), 간헐적(Intermittent), 빈번한(Frequent), 지속적(Continuation), 공기 폭발(Air Explosion)로 분류하였으며, 각 공기연행 발생 시 취수유량의 감소율 및 영향을 분석한 결과 간헐적 공기연행 발생 시 최대 약 3.75%의 취수유량 감소, 빈번한 공기연행 발생 시 취수유량은 전체적으로 10%, 최대 약 13.19% 감소하였으며, 지속적 공기연행 발생 시 발생 이후 ∆h2증가에 의한 취수유량의 증가가 거의 이루어지지 않으며, 최대 56.25%의 취수유량이 감소, 공기 폭발 발생 시 취수유량의 영향은 지속적 발생과 비슷하나 관내 공기 포집 후 유입구로 방출 시 관에 강한 충격을 주어 안정성에도 큰 영향을 미칠 것으로 판단되어, 이에 안정성 및 취수유량 감소율을 고려하여 빈번, 지속, 공기 폭발 발생 영역에서의 취수는 적합하지 않으며, 공기연행 미발생 및 간헐적 발생 영역에서의 취수 시 목표 취수유량이 1.00~4.00(㎥/s)일 때 ∆h1= 0.40m 이상, 4.00~9.30(㎥/s) 일 때 ∆h1= 0.60m 이상, 9.30~9.53(㎥/s) 일 때 ∆h1=0.80m 이상, 9.53~9.65(㎥/s) 일 때 ∆h1= 1.00m 이상에서 취수유량 감소율 3.75% 이내로 취수유량의 확보가 가능하다. 이러한 결과는 원형 다단 실린더 게이트 형식의 취수시설에 대해 취수 시 수면와류에 의한 Air Core와 그에 따른 공기연행의 발생 조건과 영향을 수리모형실험을 통해 확인함으로써 실제 운용 시 보다 안정적이고 효율적인 운용에 대한 자료로 활용될 수 있을 것으로 판단되며, 추가로 수치해석을 통한 비교 및 공기연행과 관내 공기포집 정도에 대한 연구를 통해 보다 정확한 자료제시가 가능할 것으로 판단된다.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.5
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• pp.7-14
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• 2009

A methodology of design performance estimation for the supersonic impulse turbine was investigated. Relations of similarity condition and test nozzle area ratio were derived. Comparison of efficiencies between the turbines with real nozzle and test nozzle are made numerically and experimentally. The CFD results and test result confirmed that the turbine with test nozzle was able to predict real turbine performance. In addition, design performance of the supersonic impulse turbine also could be estimated using real nozzle in air-medium test. In this case, design efficiency was found at the pressure-ratio and velocity-ratio of similarity condition of test nozzle.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2006.05a
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• pp.1149-1149
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• 2006

The leakage characteristic is an important factor in power plant. However, most of power plant have efficiency problem which is occurred leaking between high pressure steam turbine axle and stator. The labyrinth seal which is used between the main turbine axle and stator in the power plant. Because it is able to be non-contact seal and it is minimize clearance to decrease the leakage. But its actual system is too huge to experiment. Therefore, most steam turbine seal performance tests were conducted by air similarity test. This paper described a test facility and program for air similarity test of high pressure steam turbine seal. A test facility has been designed and built to evaluate leakage verification of labyrinth seal. The test facility consist of air compressor, anti-swirl labyrinth seal for 1/3 air similarity model, pressure transducer, air flow measure system, instrumentation and auxiliary system. For evaluation of steam turbine seal performance, the air similarity test of labyrinth seal leakage verification was conducted and we compared experiment data and analysis result.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.4
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• pp.55-62
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• 2009

Fracture behavior of ceramic dome port cover on air breathing engine using liquid and solid fuel propulsion system was carried out in this study. Fracture characteristics was tested and estimated using scaled model of ceramic dome port cover by Shock tube. Fracture behavior was obtained by the fracture pressure from pressure sensor and observed the scattering phenomena of fracture specimen using high speed camera. Results obtained from this study can be used in the base data of dome port cover design for an air breathing engine.