• Title/Summary/Keyword: SMILE 코드

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Simulation of Rothe Micronozzle Using DSMC method SMILE code (DSMC 방법 SMILE 코드를 이용한 Rothe 마이크로 노즐 시뮬레이션)

  • Choi, Young-In;Kim, Young-Hoon;Ok, Ho-Nam;Kim, In-Sun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.30-33
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    • 2007
  • DSMC method is now widely accepted CFD approach to compute and simulate the nozzle plume in rarefied regimes. In this study, using SMILE(Statistical Modeling in Low-density Environment) code which was developed in ITAM, Russia and coded using DSMC method, the internal flow of the Rothe micronozzle was simulated. Moreover, to show the validity of the SMILE code, the centerline temperatures according to the Reynold's number were compared with the ones obtained by the Rothe's experiment.

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Simulation of KM Plume Density Field by Residual Thrust Using DSMC Method (DSMC 방법을 사용한 KM 잔류추력 밀도장 시뮬레이션)

  • Choi, Young-In;Ok, Ho-Nam;Hong, Il-Hee
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.769-771
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    • 2011
  • The satellite payloaded on the 2nd stage of KSLV-I is planned to perform CCAM(Contamination and Collision Avoidance Maneuver) not to collide with KM(Kick Motor). At the moment, the satellite should pass through low density environment not to be contaminated by KM plume due to residual thrust. Therefore, it is necessary to predict the flow field of KM plume by residual thrust. In this paper, DSMC (Direct Simulation Monte-Carlo) method, which is widely accepted to simulate in rarefied regime, is used to compute the density field of KM plume by residual thrust and the result of DSMC simulation was compared with that of FLUENT to validate it.

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Plume Density Simulation of KM Residual Thrust Using DSMC Method (DSMC 방법을 이용한 킥모터 잔류추력 Plume Density 시뮬레이션)

  • Choi, Young-In;Kim, Keun-Taek
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.6
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    • pp.27-33
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    • 2014
  • 2nd stage of KSLV-I, NaRo-Ho, performs CCAM not to collide with Naro Science Satellite. At that moment, the satellite should pass through the Plume Density area which was generated by KSLV-I KM residual thrust. Therefore, it is necessary to predict Plume Density field of KM residual thrust and guarantee the safety of the trajectory of payload. In this paper, DSMC method was used to simulate Plume Density by KM residual thrust and the simulation showed that the trajectory of Naro Science Satellite was safe.

Coding Style Score Visualization Using Facial Expression (얼굴 표정을 이용한 코딩 스타일 점수 시각화)

  • Ji, Jeong-Hoon;Lee, Yun-Jung;Woo, Gyun
    • Journal of KIISE:Software and Applications
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    • v.37 no.7
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    • pp.578-583
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    • 2010
  • This paper presents an automated visualization system, called StyleVisualizer, which checks the coding style of source codes and visualizes the coding style score using facial expression. Our system represents some kinds of facial expressions according to the evaluated score of the code style: A smile face means that the source code follows coding standards correctly. To measure the effectiveness of the StyleVisualizer, some experiments have been conducted on two class students in an applied computer course. In the experiments, we have compared the error ratio for obeying the coding standards when the StyleVisualizer was used or not. According to the experimental results, the error ratio with the StyleVisualizer was reduced above 30% than that without it. We expect that our system can encourage the students to obey the coding standards by providing the feedback of the visualized faces corresponding to their programs, resulting in high readable programs.