• Journal of the Korean Society of Propulsion Engineers
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• v.17 no.5
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• pp.1-9
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• 2013

Variable area nozzle, where both throat and exit area vary, is required for optimal expansion and optimal nozzle shape upon operation of after-burner. Steady-state and transient analyses are carried out for each condition with and without afterburner operation and as a function of the location of the nozzle flap. Effects of that nozzle displacement on flow and thrust characteristics are analyzed from numerical results. With variable area nozzle adopted, the combustion field is variable in time, leading to periodically variable thrust. For off-design conditions, flow separation shows up due to over expansion at the flap tips and shock wave does in the nozzle due to under expansion. The undesirable phenomena can be solved by control of variable area nozzle.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.18-21
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• 2011

In this study, basic research on the pressure control using driven pintle of modulatable thruster is presented. For this purpose, pintle thruster and pintle shape was developed. The actuator model was selected by calculating pintle load using Fluent software. Preliminary unsteady experimental results show that huge pressure oscillation is occurred as the pintle approach toward nozzle wall. From the preliminary experimental results, we could see possibility of pressure control of the modulatable thruster.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.84.2-84.2
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• 2005

• Proceedings of the KIPE Conference
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• 2017.11a
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• pp.177-178
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• 2017

본 논문에서는 벅-타입 능동 전력 디커플링 회로의 단순화된 제어 방법을 위한 가변 스텝을 적용한 최적 보상 이득 알고리즘을 제안한다. 고정 스텝을 사용한 기존의 최적 보상 이득 알고리즘보다 유동적인 보상 이득 변화를 통해 DC링크 전압 리플을 효과적으로 줄일 수 있다. 기존의 방법보다 최적 보상 이득을 추적하는 시간이 줄어들어 갑작스런 부하 변동이나 이상 상황에 빠른 대응이 가능하다. 벅-타입 능동 전력 디커플링 회로는 전류 불연속 모드로 동작하며, 전류 지령치는 DC링크 전류의 1차 리플 성분에 전류 이득을 유동적으로 보상하여 생성하기 때문에 모든 구간에서 효과적으로 DC링크의 전압 리플을 줄일 수 있고 빠른 대응이 가능하다. 제안하는 가변 스텝을 적용한 최적 보상 알고리즘의 효과는 MATLAB-Simulink 시뮬레이션을 통해 검증하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.110-116
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• 2012

To analyze flow characteristics and performance of the side jet thruster with 4 shutters and rectangular nozzles, a 3-D simulation has been implemented. Numerical calculations for three rotation anlgles of the shutter, have been conducted. Internal recirculation in a chamber and asymmetric flow structure in a nozzle were observed. In addition, the more shutter rotated, the more asymmetries of flow increased, and this phenomena resulted in thrust bias. The degrees of thrust bias and thrust performance with the rotation angles of the shutter were predicted and comparisons with theoretical thrust were made.

• Journal of the Korean Society of Propulsion Engineers
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• v.17 no.2
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• pp.63-70
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• 2013

To analyze flow characteristics of the side jet thruster with 4 shutters and rectangular nozzles, a 3-D simulation has been implemented. Numerical calculations for two rotation angles of the shutter, have been conducted. Internal recirculation in a chamber and asymmetric flow structure in a nozzle were observed. In addition, the more shutter rotated, the more asymmetries of flow increased, and this phenomena resulted in thrust bias. The degrees of thrust bias and thrust performance with the rotation angles of the shutter were predicted and compared with theoretical thrust.

• 유체기계공업학회:학술대회논문집
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• 2003.12a
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• pp.167-173
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• 2003

For the measurement of mass flow rate at a wide range of operation conditions, it is required that the critical nozzle gas different diameters, since the mass flow rate through the critical nozzle depends on the nozzle supply conditions and the nozzle throat diameter. In the present study, both computational and experimental investigations are performed to explore the variable critical nozzle. Computational work using the 2-dimensional, axisymmetric, compressible Navier-Stokes equations are carried out to simulate the gas flow through variable critical nozzle. In experimnet, a cylinder with several different diameters is inserted into the critical nozzle to vary the nozzle throat diameter. Computational results are compared with the experimented ones. The computed results are in close agreement with experiment. It is found that the displacement and momentum thickness of variable critical nozzle are given as a function of Reynolds numbers. The discharge coefficient of the variable critical nozzle is predicted using an empirical equation.

• Proceedings of the Korean Information Science Society Conference
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• 1998.10c
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• pp.641-643
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• 1998

본 논문은 방대한 양의 데이터로 이루어진 삼각형 메쉬의 특성을 유지하면서 보다 적은 양의 데이터로 간략화된 메쉬를 생성해내는 기법을 제안한다. 메쉬 간략화는 기본적으로 에지 축약에 의해서 이루어지며, 에지 축약에 의해 발생하는 에러는 원본 메쉬의 점과 간략화된 메쉬의 평균 평면간의 거리를 사용하여 측정한다. 또한 본 논문에서 제안한 메쉬 간략화 기법을 사용하여 다단계의 해상도를 가지는 메쉬를 빠르게 구하기 위한 가변 해상도 모델을 구현한다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• v.9 no.2
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• pp.241-245
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• 2005

본 논문에서는 가변 전송율을 갖는 UWB 통신 시스템을 제안하고 다수의 무선 기기가 유동적으로 이동하는 파코넷 환경에서 다중접속 간섭 및 전송율에 따른 시스템 성능을 분석하였다. 또한, 전송품질을 향상시키기 위하여 Truncated Type-II Hyabrid ARQ 기법을 적용하여 불완전 채널 환경에서의 시스템 성능을 평가하였다.

• Journal of the Society of Naval Architects of Korea
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• v.45 no.1
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• pp.54-62
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• 2008

A new solution method was developed to solve the free surface flow around a hull and named as 'Variable Free Surface Panel Method'. In the method the non-linearity of the free surface boundary conditions was fully taken into account and the raised panel method was employed to effectively solve the problem. The transom stern flow was also considered and the panel on the hull was generated using the panel cutting method. Numerical calculations were performed for KCS(KRISO Container Ship) hull form and compared with the experimental data to confirm the validity of the method. The comparison with the conventional free surface panel method was also accomplished. It is confirmed that new method gives more reliable results than the conventional method.