• Title/Summary/Keyword: 불안정 조건

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형태안정성 레이온 복합소재의 염색특성에 관한 연구

  • Kim, Myeong-Sun;Park, Seong-Min;Gwon, Il-Jun;Seo, Mal-Yong;Kim, Hye-Jeong
    • Proceedings of the Korean Society of Dyers and Finishers Conference
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    • 2011.11a
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    • pp.61-61
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    • 2011
  • 비스코스 레이온(Viscose Rayon)은 목재 펄프를 원료로 한 재생섬유로서 은은한 광택과 발색성, 흡습성 등의 기능 뿐만 아니라, 천연섬유에 찾을 수 없는 Numeri감(Smoothness), Drape(처짐)성, 반발탄성을 가지고 있는 지극히 친환경적이며 자연순환형 소재로 인식, 지구온난화에 따른 CoolBiz Look 패션소재인 레이온 소재에 관심이 증대되고 있다. 한편, 레이온 소재는 수분흡수 시 강도저하, 수축과 구김, 염색 불균염 등의 문제점과 섬유공정상 생활취급상에 많은 애로를 가지고 있으며, 구성고분자가 수소결합에 의해 강고하여 "신축문제", 수분흡수시 팽윤(Swelling)에 의한 형태불안, 즉 "수축문제"가 개선해야 할 고질적 문제로 남아 있다. 또한, 습식방사에 따른 분자구조적 불안정성으로 건 습열처리시 형태불안정(치수변화율이 큼)으로 제직(준비) 및 후공정상 여러 가지 Trouble 유발과 완제품 세탁시 수축발생으로 종종 Dry Creanning해야 하는 문제점들이 내재되어 있다. 따라서 본 연구에서는 레이온 소재의 형태안정화 제품을 개발하기 위하여 복합사가공 및 염색가공 기술을 개발하고자 하며, 신축 및 복합기술에 의한 Rayon DTY, T/R 신축 및 복합기술에 의한 Rayon DTY, T/R 복합가공사를 개발, 제편직 요소기술과 최적의 전처리 조건, 다양한 염료의 종류, 염색온도 조건 등에 관한 연구를 진행하였다.

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Internal Flow characteristics of Ramjet Supersonic Intake (램제트 초음속 흡입구 내부 유동 특성)

  • Lee, Hyoung-Jin;Kim, Sei-Hwan;Jeung, In-Seuck
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.331-334
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    • 2011
  • The performance of ramjet engine is closely associated with a supersonic intake. In this study, experiments and computational simulations were conducted to observe the internal flow characteristics of the supersonic intake. The supersonic intake which have self-starting characteristics was designed and manufactured. The flow characteristics was analyzed from the experimental results using the supersonic wind tunnel testing and computational results using RANS equation and Menter's SST turbulence model. The detailed visualization results were suggested for the pseudo-shock wave of stable operations and for the inlet buzz phenomenon of unstable operations.

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Preliminary Combustion Tests in Bi-Swirl Coaxial Injectors Using Gaseous Methane/Gaseous Oxygen Propellants (기체메탄/기체산소 추진제를 이용한 동축 와류형 분사기에서의 예비 연소실험)

  • Hwang, Donghyun;Bak, Sujin;Ahn, Kyubok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.4
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    • pp.70-80
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    • 2019
  • Combustion tests using six bi-swirl coaxial injectors with different shapes and recess lengths were performed in a model combustion chamber capable of flame visualization. By utilizing gaseous methane and gaseous oxygen instead of actual propellants, the effects of injector design and experimental conditions on the flame structure and combustion stability were analyzed. It was found that not only the experimental conditions but also the injector geometry such as the recess length and orifice diameter had a considerable influence on the combustion stability. In addition, it was confirmed that the heat release pattern changed with the occurrence of combustion instability.

A Study on the Appropriate exposure time for Flood discharge measurement of Surface velocity radar (전자파표면유속계의 홍수량 측정을 위한 적정 노출시간 검토)

  • Tae Hee Lee;Jong Wan Kang;Jae Hoon Kim
    • Proceedings of the Korea Water Resources Association Conference
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    • 2023.05a
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    • pp.298-298
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    • 2023
  • 전자파표면유속계는 홍수량 측정을 위해 사용되는 비접촉식 유속계로, 전자파를 발사한 후 수표면에 반사되는 전자파의 도플러 효과를 이용하여 표면유속을 측정하는 기기이다. 국제적으로 1980년대부터 홍수량 측정의 어려움을 극복하기 위해 하천 유량측정 업무에 활용하였다. 전자파표면유속계를 이용하여 정확한 표면유속을 측정하기 위해서는 측정 위치, 방향, 노출시간, 환경 등을 고려해야 한다. 여기서 노출시간은 표면유속 측정을 위해 전자파를 흐름 상태의 수표면에 노출시키는 시간을 의미한다. 특히, 노출시간은 유속에 따라 결정되며, 빠른 유속일수록 측정에 필요한 노출시간이 짧아진다. 그러나 노출시간이 너무 짧으면 측정 유속값이 부정확하거나 불안정해질 수 있으며, 반대로 너무 길면 수위 등 측정조건이 변화하여 측정값이 부정확해질 수 있다. 따라서 홍수량 측정을 위해 전자파표면유속계의 표면유속 측정의 적정한 노출시간을 설정해야 한다. 본 연구에서는 전자파표면유속계의 적정한 노출시간 검토를 위해 안동하천실험센터에서, 표면유속 최대 4.92 m/s에서 최소 0.457 m/s 범위의 19개 유속 조건에서 노출시간을 10초에서 40초까지 5초 간격으로 변화시키며 표면유속을 측정하였다. 현재 국내외 가이드라인에서 권고하고 있는 노출시간 30초에서 측정된 표면유속과 각 노출시간에서 측정된 표면유속의 정확도 검증을 통해 유사한 값을 가지는 표면유속을 검토하여, 수위변화에 대응하여 홍수량 측정을 위한 최소 노출시간을 검토하였다.

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Experimental study of combustion stability assessment of injector (분사기의 연소 안정성 평가를 위한 실험적 방법 연구)

  • Seo, Seong-Hyeon;Lee, Kwang-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.4
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    • pp.61-66
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    • 2004
  • The objective of the present study is to develop methodology for the assessment of combustion stability of liquid rocket injectors. To simulate actual combustion occurring inside of a thrust chamber, a fullscale injector has been employed in the study, which bums gaseous oxygen and mixture of methane and propane. The main idea of the experiment is that the mixing mechanism is considered as a dominant factor significantly affecting combustion instability in a fullscale thrust chamber. A single split triplet injector has been used with an open-end cylindrical combustion chamber. The characteristics revealed by excited dynamic pressures in gaseous combustion show degrees of relative acoustic damping depending on operating conditions. Upon test results, the direct comparison between various types of injectors can be realized for the selection of the best design among prospective injectors.

A Study on the Convergence Characteristics for the Solution of Transfer Matrix Method (전달매트릭스법에 있어서 해의 수험특성에 관한 연구)

  • 김영식
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.26 no.3
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    • pp.282-287
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    • 1990
  • In this paper, it has been analysed that the stability and the effectivity of the solution using traditional transfer matrix method. And applying the false-position method to these, the convergence characteristics of the solution has been also analysed. As a result, the frontal transfer matrix method is superior to traditional transfer matrix method in the stability and the accuracy of the solution in high frequency region but in the economical efficiency and the effectivity of the calculation, traditional transfer matrix method is more desiable. Also, it is clear that $\omega-Det$ curve using the frontal transfer matrix method is discontinuous.

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Numerical Study about Behavior of an Ejecting Projectile for Varying Initial Conditions (초기 조건 변화에 따른 사출 운동체의 거동에 관한 수치적 연구)

  • Jo, Sung Min;Kwon, Oh Joon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.11
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    • pp.761-767
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    • 2019
  • In the present study, analyses of initial behavior of an air-launched projectile for varying initial conditions are performed by coupling computational fluid dynamics and 6 degrees of freedom calculations. Accuracy of the present numerical methods is validated by comparing the present result with the measured data. Launching safety analyses are carried out for various ejecting conditions by considering weight of the projectile and magnitude of front and rear ejector forces as the major parameters of initial behavior of the projectile. A response surface of the projectile launching safety is obtained in the range of the major parameters. In all the conditions of zero rear ejector force, unsafe launching behavior is observed. As the weight of the projectile decreases, the initial launching behavior becomes more unsafe.

Unchosen Cohabitation of Hannah Arendt and Precarity Politics of Judith Butler: Based on Body Politic and Ethical Obligation (한나 아렌트의 비선택적 공거와 주디스 버틀러의 프레카리티 정치학: 몸의 정치학과 윤리적 의무)

  • Cho, Hyun June
    • Cross-Cultural Studies
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    • v.48
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    • pp.361-389
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    • 2017
  • This essay examines 'precarity politics' by Judith Butler, a well-known gender theorist and queer philosopher, in Notes Towards a Performative Theory of Assembly (2015) focused on concepts as unchosen cohabitation of Hannah Arendt and unwilled proximity of Emmanuel Levinas. Butler's precarity politics is the condition of our dispossessed political beings with fundamental vulnerability and interdependency that cannot choose with whom we will live on this Earth. Butler's political ethics is twofold: on one hand, she examines significance of 'action'' the most significant vita activa in the public area, and 'plurality'' the condition-not only the necessary condition but the possible condition-for a political life suggested by Hannah Arendt in Human Condition; on the other hand, Butler reflects upon global precarity based on a diasporic precarious life in the social world towards freedom and equality. Unchosen cohabitation of plural humans on Earth, and global pervasion of precarity, that indicates "politically induced condition in which certain populations suffer from failing social and economic networks of support and become differentially exposed to injury, violence, and death," so called "differential distribution of precariousness," are practical possibilities of ethical and equal cohabitation of different ethnic groups in the social world. Ethical obligations or ethical demand to respond to others' suffering in distance and proximity originated from precarity politics, mentioned in Precarious Life, Parting Ways, and Frames of War, could be non-foundational joint of plural people living together globally. We should presume the 'reversibility' of distance and proximity in others' suffering, based on responsiveness and responsibility of others, if we want to stay attuned to the pain of others we never chose to live together. That is the significance of Butler's 'precarity politics' with 'ethical obligation' to accept 'unchosen plurality' of living population on Earth, and 'reversibility between of distance and proximity,' in her 'new plural and embodied body politics' or 'new corporeal ontology', through human primary vulnerability, fundamental interdependency, being exposed and responsive to suffering of others.

Study of Characteristics of Self-Excitation in Lifted Laminar Free-Jet Propane Flames Diluted with Nitrogen (질소 희석된 프로판 자유제트 층류부상화염에 있어서 화염 자기진동 특성에 관한 연구)

  • Yoon, Sung-Hwan;Park, Jeong;Kwon, Oh-Boong;Bae, Dae-Seok
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.4
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    • pp.399-408
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    • 2010
  • The characteristics of lifted laminar propane flames diluted with nitrogen have been investigated experimentally to elucidate self-excitation and the effects of flame curvature. Flame oscillation modes are classified as follows: oscillation induced by heat loss, a combination of oscillations induced by heat loss and buoyancy, and a combination of the oscillations induced by heat loss and diffusive thermal instability. It is shown that the oscillation induced only by heat loss is not relevant to the diffusive thermal instability and hydrodynamic instability caused by buoyancy; this oscillation is observed under all lift-off flame conditions irrespective of the fuel Lewis number. These experimental evidences are displayed through the analysis of the power spectrum for the temporal variation of lift-off height. The possible mechanism of the oscillation induced by heat loss is also discussed.

Application of Combustion Stabilization Devices to Liquid Rocket Engine (액체 로켓엔진에서 연소 안정화기구의 적용 효과)

  • Sohn, Chae-Hoon;Seol, Woo-Seok;Lee, Soo-Yong;Kim, Young-Mog;Lee, Dae-Sung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.6
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    • pp.79-87
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    • 2003
  • Application of combustion stabilization devices such as baffle and acoustic cavity to liquid propellant rocket engine is investigated to suppress high-frequency combustion instability, i.e., acoustic instability. First, these damping devices are designed based on linear damping theory. As a principal design parameter, damping factor is considered and calculated numerically in the chambers with/without these devices. Next, the unbaffled chambers with/without acoustic cavities are tested experimentally for several operating conditions. The unbaffled chamber shows the peculiar stability characteristics depending on the operating condition and it is found to have small dynamic stability margin. As a result, the acoustic cavity with the present design has little stabilization effect in this specific chamber. Finally, stability rating tests are conducted with the baffled chamber, where evident combustion stabilization is observed, which indicates sufficient damping effect.