• Title/Summary/Keyword: Supercritical fluids

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Temperature Distribution of Liquid Nitrogen Jet at Sub- and Supercritical States (아임계 및 초임계에서 액체 질소 분류의 온도 분포)

  • Lee, Hyunchang;Kim, Haisol;Cho, Seongho;Sung, Hong-Gye;Yoon, Youngbin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.1
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    • pp.1-6
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    • 2018
  • Temperatures of cryogenic nitrogen jet inside an injector and at three different downstream positions (0.9, 10.6, and 28.1d) were measured with thermocouples in sub- and supercritical states. The jet temperature decreased while cooling the supply line and injector. The jet experienced from flash boiling, boiling and then no boiling according to decreasing temperature. As an analogy to flash-boiling at the subcritical state, pseudo-flash boiling has been assumed considering the existence of pseudo-boiling at the supercritical state. By showing an area where the temperature did not increase downstream, the plausibility of pseudo-flash boiling is proposed.

Visualization of Doublet Impinging Jet Spray in Supercritical Mixed Hydrocarbon Fluid (초임계 탄화수소계열 혼합유체의 이중 충돌 제트 분무 가시화)

  • Song, Juyeon;Choi, Myeung Hwan;An, Jeongwoo;Koo, Jaye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.4
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    • pp.53-58
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    • 2021
  • Based on surrogate model, a hydrocarbon mixture was analyzed by visualizing the impinging break up mechanism in subcritical and supercritical conditions. Decane and methylcyclohexane with different critical pressures and temperatures were selected as experimental fluids. The impinging injector was installed inside the chamber, and the spray was visualized through a speed camera in subcritical and supercritical conditions. The injection condition of the mixture and chamber was kept constant at Pr(P/Pc) = 1, and Tr(T/Tc) was increased from 0.48 to 1.02. As Tr increased, the spray angle increased, and the sheet length decreased as the properties of the mixture reached each critical point. In addition, when the mixture approached the near critical point, it was shown that the change in density gradient was largely observed out of the impinging break up mechanism.

Micronization of Triclosan Using Supercritical Fluids (초임계 유체를 이용한 트리클로산의 미세입자 제조)

  • Shin, Moon-Sam
    • Proceedings of the KAIS Fall Conference
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    • 2012.05a
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    • pp.360-362
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    • 2012
  • 본 논문에서는 의약품, 화장품, 생활용품에서 널리 사용되는 약물인 트리클로산에 대해 초임계 유체를 이용하여 미세화공정이 연구되었다. 낮은 임계온도와 임계압력의 조건을 고려하여 초임계 이산화탄소를 선정하였고, 초임계 이산화탄소와의 용해도를 고려하여 초임계 용액 급속팽창공정이 선정되었다. 본 연구에서 입자크기에 영향을 미치는 온도와 압력효과가 검토되었고 상평형자료에 의해 해석되었다.

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Subsonic/Transonic Airfoil Design Using an Inverse Method (Inverse 기법을 이용한 아음속/천음속 익형 설계)

  • Lee Jae Woo;Lee Young-Ki;Byun Yung-Hwan
    • 한국전산유체공학회:학술대회논문집
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    • 1998.05a
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    • pp.61-66
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    • 1998
  • An inverse method for the subsonic and transonic airfoil design was developed using the Euler equations. Two testcases were performed. One was a design of the supercritical airfoil, aiming to be used for the Korean mid-sized (100 passengers class) transport aircraft. The other was the design of an airfoil showing a good cruising performance (L/D ratio) in the high subsonic/transonic flow regimes. These testcases demonstrated the efficiency and the robustness of the developed method.

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Micronization of Salicylic Acid Using Supercritical Fluids (초임계 유체를 이용한 살리실산의 미세입자 제조)

  • Shin, Moon-Sam
    • Proceedings of the KAIS Fall Conference
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    • 2011.05a
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    • pp.482-484
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    • 2011
  • 본 논문에서는 화장품과 생활용품에서 널리 사용되는 약물인 살리실산에 대해 초임계 유체를 이용하여 미세화공정이 연구되었다. 낮은 임계온도와 임계압력의 조건을 고려하여 초임계 이산화탄소를 선정하였고, 초임계 이산화탄소와의 용해도를 고려하여 초임계 용액 급속팽창공정이 선정되었다. 본 연구에서 입자크기에 영향을 미치는 온도와 압력효과가 검토되었고 상평형자료에 의해 해석되었다.

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Micronization of Cosmeceutical Biocide Using Supercritical Fluids (초임계 유체를 이용한 약용화장품 항균제의 미세입자 제조)

  • Shin, Moon-Sam
    • Proceedings of the KAIS Fall Conference
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    • 2011.12a
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    • pp.361-363
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    • 2011
  • 본 논문에서는 의약품, 화장품, 생활용품에서 널리 사용되는 약물인 히토키치올에 대해 초임계 유체를 이용하여 미세화공정이 연구되었다. 낮은 임계온도와 임계압력의 조건을 고려하여 초임계 이산화탄소를 선정하였고, 초임계 이산화탄소와의 용해도를 고려하여 초임계 용액 급속팽창공정이 선정되었다. 본 연구에서 입자크기에 영향을 미치는 온도와 압력효과가 검토되었고 상평형자료에 의해 해석되었다.

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Subsonic/Transonic Airfoil Design Using an Inverse Method (Inverse 기법을 이용한 아음속/천음속 익형 설계)

  • Lee Young-Ki;Lee Jae-Woo;Byun Yung-Hwan
    • Journal of computational fluids engineering
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    • v.3 no.1
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    • pp.46-53
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    • 1998
  • An inverse method for the subsonic and transonic airfoil design was developed using the Euler equations. Two testcases were performed. One was a verification of the method using the supercritical airfoil of the Korean mid-sized (100 passengers class) transport aircraft. The other was the design of an airfoil showing a good cruising performance (L/D ratio) in the high subsonic flow regime. These testcases demonstrated the efficiency and the robustness of the design method in the present study.

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A Study on the Variable Condition Debinding Process in Supercritical CO2 for Removing Binder from Thick Ceramic Injection Molded Parts (두꺼운 세라믹 사출성형체로부터 효율적인 결합제 제거를 위한 초임계 CO2 가변조건 탈지공정 연구)

  • Kim, Hyung-Kun;Yim, Joon-Hyuk;Kim, Hyung-Soo;Lim, Jong-Sung
    • Clean Technology
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    • v.18 no.2
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    • pp.155-161
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    • 2012
  • The purpose of this study is to remove paraffin wax binder effectively from powder injection molded part using supercritical fluids in powder injection molding process. For a thin powder injection molded part about 1-2 mm thickness, paraffin wax binder can be removed rapidly without any defect by traditional supercritical extraction process which has fixed high temperature and pressure condition. But, for a thick powder injection molded part, there are limitations in removing paraffin wax binder by the fixed high process condition because crack occurs at the beginning step. Therefore, here we studied variable condition debinding process that starts with mild process condition at the beginning step and then increase the process conditions simultaneously at each step. To find out the initial process condition that has the highest extraction yield without any defect for each sample thickness, we investigated various supercritical debinding conditions using 1-4 mm thickness ceramic injection molded sample. By using the variable condition debinding process that starts with the initial process condition at the first step and then increasing process conditions simultaneously at each step (temperature from 333.15 to 343.15 K, pressure from 12 to 27 MPa, and $CO_2$ flow rate from 1.5 to 10 L/min), over 95% of paraffin wax binder was removed from the 4 mm thick (10 mm diameter) ceramic injection molded disk samples within 5 hours.