• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.5
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• pp.10-19
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG($CH_4$)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.367-376
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG(CH4)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.231-238
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• 2010

Combustion stability rating tests under condition low pressure of a 75-$ton_f$ liquid rocket engine(LRE) thrust chamber were carried out. Mixing head with decreased number of injectors than that of the other but with the same mass flow rate to the combustion chamber showed self-oscillation instability in chamber pressure of 30 bar. The other combustion chamber with increased number of injectors showed that high frequency combustion stability was maintained under condition of same pressure, but self-oscillation instability was generated in chamber pressure of 20 bar which can be considered as stability boundary region of this mixing head.

• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.5
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• pp.92-100
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• 2010

Combustion stability rating tests of 75-tonf-class thrust chamber for technology demonstration were carried out at a low pressure. Two kinds of mixing heads were used in this study. One of them has injectors of 631 and the other has injectors of 721. Mixing head with injectors of 631 showed a self-oscillation instability at the chamber pressure of 30 bar. Mixing head with injectors of 721 showed that a high frequency combustion stability was maintained under the same pressure and the same mass flow rate. But mixing head with injectors of 721 generated a self-oscillation instability at the chamber pressure of 20 bar and it was found that stability boundary region was changed due to the configuration of a mixing head from these results.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.259-264
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• 2005

Measurements of heat release are very important for controling combustion instabilities, which are closely connected with combustion instabilities. $OH^{\ast}$ images were acquired through a ICCD in this study, which were in use as indicating index of the reacting region, global and local heat release rate in the lean premixed combustion. The objectives of this study are to see the effect of equivalence ratio on global heat release rate and local Rayleigh index distribution. The local Rayleigh index distribution was acquired by information from central section of flame. This information was from the line-of-sight images which were inverted by the Abel de-convolution. In each condition, the mean value of heat release increased exponentially with equivalence for a periodic time. Local Rayleigh index distribution cleary showed the region of amplifying or damping the combustion instability as the equivalence ratio increased. This could provide an insight on the region of combustion instability and the structure of flames on the equivalence ratio.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.437-444
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• 2005

Experiments were carried out in an atmospheric pressure, lab-scale gas turbine combustor to see the effect of partial premixing on unstable flame structure and Nox emission characteristics. The swirl angle is 45 deg., fuel-air mixing degrees were varied 0, 50 and 100% respectively at equivalence ratio ranging from 0.53 to 0.79. The evolution of phased-locked OH chemiluminescence images were acquired with an ICCD. NOx emission characteristics were also investigated at each experimental condition. The effect of the fuel-air mixing degree on the flame structure was obtained from phase-locked $OH^*$ images. And it was obtained from local heat release characteristics that the information about the region which the combustion instability was amplified or damped. It also could be confirmed that $\sigma$ has greatly influence on NOx emission characteristics at lean regimes. It would be expected that it could provide invaluable data for understanding the mechanism of combustion instability.

• Korean Journal of Child Education & Care
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• v.19 no.1
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• pp.59-73
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• 2019

Objective: The purpose of this study was to investigate the moderating effect of mothers' play support beliefs on the relation between mothers' insecure attachment and children's playfulness. Methods: The research participants of this study include 254 children aged 3 to 5, who attended kindergartens and day care centers located in Seoul, Gyeonggi and Chung-cheong, and their 254 mothers. For data analyses, descriptive statistics, Pearson's correlation and hierarchical multiple regression were conducted using SPSS 23.0 program. Results: First, there was negative association between mothers' insecure attachment and play support beliefs. Social spontaneity and expression of joy were negatively related to mothers' insecure attachment. However, mothers' play support beliefs showed positive associations with children's playfulness, particularly including children's physical spontaneity and expression of joy. In addition, mothers' play support beliefs moderated the relation between mothers' insecure attachment and children's expression of joy. However, the beliefs did not moderate the relation between mothers' insecure attachment and other playfulness traits. Conclusion/Implications: The findings of the present study indicate that mothers' understanding of the importance of play may buffer the adverse effect of mothers' insecure attachment on children's capabilities of expressing their sense of pleasure.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.68-77
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• 2017

High-frequency combustion instability results from a feedback coupling between the unsteady heat release rate and the acoustic waves formed resonantly in the combustion chamber. It can be modeled as thermoacoustic problems with various degrees of the assumptions and simplifications. This paper presents numerical analysis of self-excited combustion instabilities in a variable-length lean-premixed combustor and designs of passive control devices such as baffle and acoustic resonators in a framework of 3-D FEM Helmholtz solver. Nonlinear behaviors such as steep-fronted shock waves and a finite amplitude limit cycle are also investigated with a compressible flow simulation technique.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.268-271
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• 2006

Combustion response function of a solid propellant is measured and calculated to study and model the feedback process between acoustic waves and combustion field. Standard Pulsed DB/AB method and related one-dimensional approximate analysis of T-burner are used to obtain the response function at a driving natural frequency. The problems related with simultaneous ignition of propellant samples are also mentioned and treated.

• Proceedings of the Optical Society of Korea Conference
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• 2000.02a
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• pp.142-143
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• 2000

레이저는 입력을 증가시킴에 따라 레이저의 꺼짐 상태에서 레이저의 켜짐 상태로 전이한다. 그러나 그 전이 현상에 대해서는 아직 밝혀진 바가 없다. 이때까지 이 현상은 처음 자발전이의 빛이 점점 유도전이로 바뀌며 그 빛이 점점 세어져 레이저의 출력이 생기기 시작하고 이것이 레이저 입력의 증가에 따라 연속적으로 발전하는 것으로 알려져 왔다. 그러나 이러한 결과에 반대되는 결과들이 최근 밝혀지고 있다[1-2]. 그것은 이산화탄소 레이저에서 이득을 변조시키면 방전이 불안정해지고 그 결과 레이저의 출력도 불안정해 지는데 특히 발진 문턱 근처에서 레이저의 출력은 불규칙 적으로 레이저의 출력이 사라지는 현상이 생긴다는 것이다[1]. 또 다른 하나는 cw Nd:YAG 레이저를 아크 램프로 여기시켜 발진시키면 발진 문턱 근처에서 이 레이저의 출력도 불규칙적으로 레이저의 출력이 사라지는 것으로 나타난다[2]. 이 현상은 레이저의 입력을 증가시킴에 따라 레이저의 꺼짐 상태에서 발진 상태로 전이할 때 그 중간에 불규칙적인 레이저의 꺼짐 상태가 존재한다는 것이 된다. 이 현상이 비선형 동력학의 특이한 현상 중의 하나인 on-off 간헐성임[3]이 밝혀졌다. (중략)