• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.3
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• pp.38-44
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• 2003

In this study, a performance model of the smart UAV propulsion system with ducts, tip jets and variable main nozzle, which has flight capability of the rotary wing mode for the take-off/landing and low speed forward flight as well as the fixed wing mode for high speed forward flight, has been newly developed With the proposed model, steady-state performance analysis was performed at various flight modes such as rotary wing mode, fixed wing mode, compound ing mode and altitude as well as at flight speed conditions. In investigation of performance analysis. it was noted that the operational capability of the propulsion system was limited due to the duct losses depending on each flight mode, and the limitation with the altitude variation case had much greater than that with the flight speed variation case.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.1
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• pp.18-22
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• 2006

Hydrodynamic performance test was conducted for a fuel pump of a liquid rocket engine turbopump. The pump driven by an electric motor was tested using water. It is experimentally shown that the inducer had very small effect on the pump's head and efficiency but great effect on the pump's cavitation performance. Additionally, inducer test was carried out to investigate the effect of the inducer on the pump in detail, and it was found that the pump reached a critical cavitation number when the inducer head dropped by 55%.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.245-249
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• 2007

In this study a model-based diagnostic method using the Neural Network was proposed for PW206C turbo shaft engine and performance model was developed by SIMULINK. Fault and test database to build the NN was obtained at various off-design operating range such as flight altitude, flight Mach number and gas generator rotational speed variation. According to the fault detection analysis results, it was confirmed that the proposed fault detection method could find well the fault of compressor, compressor turbine and power turbine at on-design point as well as off-design point conditions.

• Journal of the Korean Institute of Intelligent Systems
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• v.20 no.6
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• pp.768-773
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• 2010

This paper presents the performance verification of the optimal state feedback controller via inverted pendulum systems. The proposed method generates the optimal control inputs satisfying both the constrained input and the performance specification. In addition, it reduces the steady-state error by adopting the integral control technique. In order to verify the performance of the proposed method, we apply both the proposed method and the general state feedback control to an inverted pendulum, CEM-IP-01 in the experiment.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.3
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• pp.29-34
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• 2007

In this study a model-based diagnostic method using the Neural Network was proposed for PW206C turbo shaft engine and performance model was developed by SIMULINK. Fault and test database to build the NN was obtained at various off-design operating range such as flight altitude, flight Mach number and gas generator rotational speed variation. According to the fault detection analysis results, it was confirmed that the proposed fault detection method could find well the fault of compressor, compressor turbine and power turbine at on-design point as well as off-design point conditions.

• The KSFM Journal of Fluid Machinery
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• v.11 no.5
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• pp.7-14
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• 2008

Open channel type regenerative pump has been used in various industrial fields. It generates high pressure with low flow rate. However, it has low efficiency because of its complex flow pattern, We studied performance experiments and 3D numerical flow analysis of a regenerative pump. Through the numerical analysis, we could get the internal flow pattern and profile of a regenerative pump. Also, we examined leakage flow effects due to the gap between casing and impeller and stripper clearance. For the numerical analysis verification, we performed experiments and they had similar tendency at the design point.

• Proceedings of the Korean Institute of Building Construction Conference
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• 2009.05c
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• pp.61-64
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• 2009

The number of apartment houses has accounted for more than 50% of all domestic residential types in Korea since 1980s. However, the apartment house has environmentally disadvantageous conditions such as highly residential-density and potential falls by children aged seven years and under through windows. In this study, we aim to suggest some ideas to improve domestic performance assessment methods and criteria of window Insect screens for protection on security and fall prevention by analyzing domestic standard with several overseas codes related to the screens for windows.

• Proceedings of the Korean Information Science Society Conference
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• 2005.11a
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• pp.1033-1035
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• 2005

일반적으로 기존의 Ad-hoc 무선 네트워크 환경에서의 라우팅 정책은 가장 빠르게 데이터를 전송할 수 있는 경로를 찾는 것이 목적이었다. 그러나 한정된 전력을 가진 노드로 구성한 네트워크에서 각 노드의 잔여전력량을 무시하고 라우팅 경로를 설정하면 수명을 다한 특정 노드로 인해 네트워크의 성능이 저하되는 문제점이 발생한다. 따라서 본 논문에서는 각 노드의 생존시간을 최대한 보장할 수 있도록 라우팅 경로를 선택하여 네트워크의 성능 저하를 최소화하는 라우팅 정책을 제안한다. 이 정책은 기존의 테이블 기반 라우팅 정책에 두 가지 metric을 더하여 잔여 전력이 많은 노드를 포함하는 경로를 설정할 수 있게 해 준다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.4
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• pp.382-388
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• 2004

The hydraulic and suction performance of an inducer varies sensitively with the inducer geometry and this paper deals with solidity as the inducer geometry parameter. The typical performance characteristics of a basic inducer was investigated and tests with another three inducers of which the solidity is different from each other were performed, so the effect of solidity on the inducer performance was experimentally investigated. For a fixed flow coefficient, required NPSH of the inducer did not follow the conventional similarity rule, so this paper suggested another empirical formula. The hydraulic and suction performance was measured at four cases of the tip solidity ranged from 1.32 to 2.76. As long as the tip solidity had the value above 1.84, the hydraulic and suction performance of the inducer increased with decrease in the tip solidity. With further decrease in the tip solidity up to 1.32, however, inducer head decreased and the suction performance dropped sharply.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05b
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• pp.362-367
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• 1996

CANDU-6형 원자력발전소인 월성 2,3,4호기 비상급수계통의 성능을 평가하기 위하여 설계기능 수행과 관련된 변수로서 격납건물내 집수조(sump) 온도와 열수송계통으로 주입되는 냉각재온도를 사용한 분석을 수행하였다. 이 온도들은 NTU(Number of Transfer Unit)방법을 이용한 비상노심 냉각계통 열교환기의 열전달속도와 열전달계수의 해석을 열평형관계식과 함께 조합한 프로그램을 사용하여 계산하였다. 또한 증기발생기 급수량과 추후 수조에 공급되는 보충수에 대한 설계요건을 검토하였다. 이러한 변수와 설계요건은 비상급수계통이 발전소 정상 열제거기능 상실후 노심의 붕괴열제거에 유효한 열침원으로서의 기능을 수행함을 보여 주었다. 또 격납건물의 건전성 유지와 관련된 집수조내 최고온도가 허용치 이하로 유지되었다.