• 제목/요약/키워드: PLIF

검색결과 128건 처리시간 0.022초

CANDU-6 감속재 탱크 모형의 유동장 전산해석 및 예비측정 (Computational Flow Analysis and Preliminary Measurement for the CANDU-6 Moderator Tank Model)

  • 차재은;최화림;이보욱;김형태
    • 한국가시화정보학회지
    • /
    • 제10권3호
    • /
    • pp.30-36
    • /
    • 2012
  • We are planning to construct a scaled-down moderator facility to simulate the CANDU-6 moderator circulation phenomena during steady state operating and accident conditions. In the present work a preliminary experiment using a 1/40 scaled-down moderator tank has been performed to investigate the anticipated problems of the flow visualization and measurement in the planning scaled-down moderator facility. We shortly describe CFD analysis result for the 1/40 scaled-down test model and the flow measurement techniques used for this test facility under isothermal flow conditions. The Particle Image Velocimetry (PIV) method is used to visualize and measure the velocity field of water in a transparent Plexiglas tank. Planar Laser Induced Fluorescence (PLIF) technique is used to evaluate the feasibility of temperature field measurement in the range of $20-40^{\circ}C$ of water temperature using an one-color method.

DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 Part II : 반응 유동장 (Unsteady Three-Dimensional Analysis of Transverse Fuel Injection into a Supersonic Crossflow using Detached Eddy Simulation Part II : Reacting Flowfield)

  • 원수희;정인석;최정열
    • 한국항공우주학회지
    • /
    • 제37권9호
    • /
    • pp.879-888
    • /
    • 2009
  • 초음속 주 유동내 수소의 수직분사에 의한 비정상 반응 유동장에 대한 3차원 수치해석이 DES 난류 모델과 상세 화학반응 모델을 이용하여 수행되었다. 난류 반응 유동의 물리적 현상을 이해하기 위하여 해석 및 실험 결과를 비교하였다. 계산에 의해 구해진 OH 분포는 실험의 OH-PLIF 결과를 잘 모사하고 있다. 반면, 점화 지연 시간은 계산과 실험 사이에 차이를 보이고 있으며, 이는 실험적 계측의 한계에 기인하는 것으로 생각된다. RANS 및 DES 계산 결과의 비교로부터 간헐 현상을 확인하였으며, 유선을 따른 온도 분포 및 중첩된 OH 질량 분율을 통해 시 공간적 간헐 현상을 정량적으로 측정하였다.

동축공기 수소 난류확산화염에서의 화염안정성에 대한 실험적 연구 (Study of Hydrogen Turbulent Non-premixed Flame Stabilization in Coaxial Air Flow)

  • 오정석;김문기;최영일;윤영빈
    • 대한기계학회논문집B
    • /
    • 제32권3호
    • /
    • pp.190-197
    • /
    • 2008
  • It was experimentally studied that the stabilization mechanism of turbulent, lifted jet flames in a non-premixed condition to reveal the newly found liftoff height behavior of hydrogen jet. The objectives are to report the phenomenon of a liftoff height decreasing as increasing fuel velocity, to analyse the flame structure and behavior of the lifted jet, and to explain the mechanisms of flame stability in hydrogen turbulent non-premixed jet flames. The hydrogen jet velocity was changed from 100 to 300m/s and a coaxial air velocity was fixed at 16m/s with a coflow air less than 0.1m/s. For the simultaneous measurement of velocity field and reaction zone, PIV and OH PLIF technique was used with two Nd:Yag lasers and CCD cameras. As a result, it was found that the stabilization of lifted hydrogen diffusion flames is correlated with a turbulent intensity and Karlovitz number.

Sequential Changes of Plasma C-Reactive Protein, Erythrocyte Sedimentation Rate and White Blood Cell Count in Spine Surgery : Comparison between Lumbar Open Discectomy and Posterior Lumbar Interbody Fusion

  • Choi, Man Kyu;Kim, Sung Bum;Kim, Kee D.;Ament, Jared D.
    • Journal of Korean Neurosurgical Society
    • /
    • 제56권3호
    • /
    • pp.218-223
    • /
    • 2014
  • Objective : C-reactive protein (CRP) and erythrocyte sedimentation rate (ESR) are often utilized to evaluate for postoperative infection. Abnormal values may be detected after surgery even in case of non-infection because of muscle injury, transfusion, which disturbed prompt perioperative management. The purpose of this study was to evaluate and compare the perioperative CRP, ESR, and white blood cell (WBC) counts after spine surgery, which was proved to be non-infection. Methods : Twenty patients of lumbar open discectomy (LOD) and 20 patients of posterior lumbar interbody fusion (PLIF) were enrolled in this study. Preoperative and postoperative prophylactic antibiotics were administered routinely for 7 days. Blood samples were obtained one day before surgery and postoperative day (POD) 1, POD3, and POD7. Using repeated measures ANOVA, changes in effect measures over time and between groups over time were assessed. All data analysis was conducted using SAS v.9.1. Results : Changes in CRP, within treatment groups over time and between treatment groups over time were both statistically significant F(3,120)=5.05, p=0.003 and F(1,39)=7.46, p=0.01, respectively. Most dramatic changes were decreases in the LOD group on POD3 and POD7. Changes in ESR, within treatment groups over time and between treatment groups over time were also found to be statistically significant, F(3,120)=6.67, p=0.0003 and F(1,39)=3.99, p=0.01, respectively. Changes in WBC values also were be statistically significant within groups over time, F(3,120)=40.52, p<0.001, however, no significant difference was found in between groups WBC levels over time, F(1,39)=0.02, p=0.89. Conclusion : We found that, dramatic decrease of CRP was detected on POD3 and POD7 in LOD group of non-infection and dramatic increase of ESR on POD3 and POD7 in PLIF group of non-infection. We also assumed that CRP would be more effective and sensitive parameter especially in LOD than PLIF for early detection of infectious complications. Awareness of the typical pattern of CRP, ESR, and WBC may help to evaluate the early postoperative course.

Visualizing Detonation Waves

  • Shepherd, Joseph E.
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2006년도 제33회 KOSCO SYMPOSIUM 논문집
    • /
    • pp.9-11
    • /
    • 2006
  • Visualization has played an essential role in the development of our understanding of the complex unsteady flows associated with the initiation, propagation, and extinction of detonation waves. These methods and application to various aspects of detonation are illustrated by results obtained in my laboratory, particularly using combinations of the PLIF technique with other methods. Examples shown will include detonation initiation by projectiles, diffraction over ramps and steps, diffraction out of tubes, detonation implosion, and the cellular structure of detonation waves.

  • PDF

PLIF 기법을 이용한 액체 로켓용 F-O-O-F 인젝터의 혼합특성 연구

  • 정기훈;윤영빈
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2000년도 제14회 학술강연논문집
    • /
    • pp.2-2
    • /
    • 2000
  • 액체연료를 사용하는 엔진의 인젝터에 대한 연구는 연소효율에 중대한 영향을 미치는 분무 액적의 크기 및 분포 특성 연구에 초점을 두어왔다. 그러나 액체 로켓 엔진은 고온, 고압의 연소실 내에서 액체상태의 연료 및 산화제 액적이 매우 빠르게 기화되기 때문에, 미립화 특성 보다는 연료와 산화제의 혼합특성이 연소효율을 결정하는 변수로 작용하게 된다. 또한 분사된 액체 추진제는 미립화 단계 이전에 기화되어 초기 화염을 형성하므로, 분사 직후의 연료/산화제의 혼합과정을 이해하는 것은 상당히 중요하다.

  • PDF

하부 요추 방출 골절의 수술방법 결정시 고려 요인들 (Factors in Selection of Surgical Approaches for Lower Lumbar Burst Fractures)

  • 장태안;김종문
    • Journal of Korean Neurosurgical Society
    • /
    • 제29권8호
    • /
    • pp.1055-1062
    • /
    • 2000
  • Objectives : Burst fracture of the lower lumbar spine(L3-L5) is rare and has some different features compare to that of thoracolumbar junction. Lower lumbar spine is flexible segments located deeply, and has physiologic lordosis. All of these contribute to making surgical approach difficult. Generally, lower lumbar burst fracture is managed either anteriorly or posteriorly with various fixation and fusion methods. But there is no general guideline or consensus regarding the proper approach for such lesion. We have tried to find out the influencing factors for selecting the surgical approach through the analysis of lower lumbar burst fractures treated for last 4 years(1994.3-1998.3). Method : This study includes 15 patients(male : 10, female : 5, age range 20-59 years with mean age of 36.7 years, L3 : 8 cases, L4 : 5 cases, L5 : 2 cases). Patients were classified into anterior(AO) and posterior operated(PO) groups. We investigated clinical findings, injured column, operation methods, and changes in follow-up radiologic study (kyphotic angle) to determine the considerable factors in selecting the surgical approaches. Results : There were 5 AO and 10 PO patients. Anterior operation were performed with AIF with Kaneda or Z-plate and posterior operation were done with pedicle screw fixation with PLIF with cages or posterolateral fusion. Canal compression was 46.6% in AO and 38.8% in PO. The degree of kyphotic angle correction were 10.7 degree(AO) and 8.5 degree(PO), respectively. There was no statistical difference between anterior and posterior operation group. All patients showed good surgical outcome without complications. Conclusion : Anterior operation provided good in kyphotic angle correction and firm anterior strut graft, but it difficulty arose in accessing the lesions below L4 vertebra. While posterior approach showed less correction of kyphotic angle, it required less time and provided better results for accompanied adjacent lesion and pathology such as epidural hematoma. The level of injury, canal compression, biomechanics, multiplicity, and pathology are considered to be important factors in selection of the surgical approach.

  • PDF

부상된 동축공기 수소 난류확산화염에서의 화염안정화 특성 (Characteristics of Stabilization Point in Lifted Turbulent Hydrogen Diffusion Jet with Coaxial Air)

  • 오정석;김문기;윤영빈
    • 한국항공우주학회지
    • /
    • 제36권4호
    • /
    • pp.352-356
    • /
    • 2008
  • 수소제트와 동축공기를 사용한 본 연구에서, 난류확산화염의 화염안정성 특징을 실험적으로 수행하였다. 목적은 연료속도 증가에 따라 감소하는 부상화염길이의 경향을 보고하고, 부상 메커니즘을 포함한 화염구조를 분석하는 것이다. 수소연료는 100에서 300 m/s 사이에서 조절되었으며, 이때 동축공기는 16 m/s 고정되고, 주위류는 0.1 m/s 이하로 유지되었다. 유동장과 연소장 동시측정을 위하여, 두 대의 Nd:Yag 레이저와 CCD 카메라를 이용하여 PIV와 OH PLIF 기법이 사용되었다. 결론적으로 난류화염전파속도는 난류강도에 비례하였으며, 제트 레이놀즈수의 0.017승에 비례하였다.

초음속 공기 유동장에서의 수소 확산 화염 특성에 대한 연구 (The Characteristics of Unconfined Hydrogen Diffusion Flames in Supersonic Air Flows)

  • 김제흥;심재헌;김지호;윤영빈
    • 한국추진공학회지
    • /
    • 제4권4호
    • /
    • pp.78-86
    • /
    • 2000
  • Mach 1.8의 동축공기를 갖는 수소 난류 화산 화염의 특성을 이해하는 것이 본 연구의 목적이다. 화염길이와 연료유동의 자취에 대한 직접사진, Acetone PLIF, Mie scattering, 수치해석법을 이용하여 화염의 구조를 분석하였다. 연료의 유속를 고정시켰을 때, 공기의 유속 증가에 따른 변화를 측정하였다. 아음속 화염의 길이는 급격히 감소한 반면, 초음속 화염의 길이는 완만하게 증가하였다. 또한 연료 노즐 립의 두께 변화에 따른 화염의 소염 특성을 관찰하였다. 노즐 립의 두께에 따라 화염 안정성이 증가하였는데 이는 초음속 화염의 안정화를 위한 최소 두께 값이 존재함을 나타낸다. 유동장 구조를 분석한 결과, 연료 제트가 고압영역에 가로 막혀서 축방향 모멘텀을 잃고, 저산란 영역이 만들어지는 것을 확인하였다. 또한, 모멘텀을 잃은 연료가 재순환 영역을 따라 순환하면서 긴 체류시간을 갖기 때문에 예혼합 영역이 만들어 졌음이 밝혀졌다.

  • PDF

초음속 유입 유동 조건에 따른 공동을 포함한 덕트 내 초음속 연소 현상에 관한 실험적 연구 (Experimental Study on Supersonic Combustion Phenomena in the Cavity Duct by the Supersonic Inflow Conditions)

  • 정은주;정인석
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2006년도 제33회 KOSCO SYMPOSIUM 논문집
    • /
    • pp.209-219
    • /
    • 2006
  • The supersonic combustion experiments are carried out using T3 free-piston shock tunnel. Different shock tube fill pressures have various inflow conditions. $15^{\circ}$ inclined hydrogen fuel injection is located before the cavity. Oblique shock is generated at the trailing edge of the cavity and reflects off the top and bottom wall. For non-reacting flow, static pressures in low equivalence ratio are similar to those in no fuel injection. As equivalence ratio is increased, static pressures are increased in the duct. In the similar equivalence ratio, static pressures are increased when total enthalpy is decreased. For reacting flow, the flame is occurred near the cavity. The combustion is weak locally in the middle of the duct. The up and down pressure distribution in the duct means that the supersonic combustion is generated.

  • PDF