• 제목/요약/키워드: Impinging Plate

검색결과 228건 처리시간 0.028초

PIV를 이용한 삼중 제트의 유동 특성에 관한 연구 (A Study on the Flow Characteristics of the Triple Jets Using Particle Image Velocimetry)

  • 이명재;윤순현;김동건;김문경
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2005년도 추계학술대회 논문집
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    • pp.28-35
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    • 2005
  • Experiments were conducted to show the characteristics of the flow on triple parallel plane impinging jets. Measurements of mean velocity components and turbulent intensities were carried out with a particle image velocimetry(PIV) to investigate the flow field generated by the air issued from three identical plane parallel nozzles and mixed with the ambient air. The measurements range of these experiments were Reynolds number of 5000 and 1000 based on the nozzle width and the case of nozzle-to-plate distances were two times, six times and ten times the width of the nozzle. Results show that recirculation region of Re=5000 is the stronger than that of Re=1000. Therefore, velocity loss of centerline for Re=5000 that shows strongly recirculation region takes effect greatly.

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Engineering Applications of Jet Impingement Associated with Vertical Launching System Design

  • Hong, Seung-Kyu;Lee, Kwang-Seop
    • International Journal of Aeronautical and Space Sciences
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    • 제3권2호
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    • pp.67-75
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    • 2002
  • In the course of missile system design, jet plume impingement is encountered in designing airframe as well as launchers, requiring careful investigation of its effect on the system. In the present paper, recent works on such topic are presented to demonstrate usefulness of CFD results in helping design the hardware. The jet impinging flow structure exhibits such complex nature as shock shell, plate shock and Mach disk depending on the flow parameters. The main parameters are the ratio of the jet pressure to the ambient pressure and the distance between the nozzle and the wall. In the current application, the nozzle contour and the pressure ratio are held fixed, but the jet impinging distance is varied to illuminate the characteristics of the jet plume with the distance. The same methodology is then applied to a complex vertical launcher system (VLS), capturing its flow structure and major design parameter. These applications involving jets are thus hoped to demonstrate the usefulness and value of CFD in designing a complex structure in the real engineering environment.

저속 유동용 Pressure Sensitive Paint 기술개발과 응용 (Development of Pressure Sensitive Paint (PSP) Technique for Low-speed Flows and Its Application)

  • 강종훈;이상준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.688-693
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    • 2003
  • The PSP technique has been used to measure pressure distribution on a model surface quantitatively. The objective of this study is to develop PSP technique which can be applied to low-speed flows. Four different PSP formulations including two porphyrins (PtOEP and PtTFPP) and two polymers (Poly(TMSP) and RTV-118) were tested and the performance of each combination was checked. In the static calibration, the luminescent intensity of the PSP coatings was measured from 0kPa to 11kPa with 0.5, 1, 2kPa increments. Among 4 PSP formulations tested, the combination of PtOEP and RTV-118 shows the best performance. The PSP technique was applied to an oblique impinging jet to measure the pressure field distribution on the impinging plate.

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초음속 충돌 제트에 대한 비정상 유동 해석 (Unsteady Flow Analysis of Supersonic Impinging Jet)

  • 김성인;박승오;홍승규
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2002년도 춘계 학술대회논문집
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    • pp.23-28
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    • 2002
  • TNumerical simulations of the supersonic impinging jet flows are carried out using the 3D Navier-Stokes code. This paper is focuses on the unsteady flow features associated with stagnation bubbles and other oscillatory behavior. The 3D code was validated by reproducing the results of Lamont's experiments. Computation is carried out for the cases in which the unsteadiness of the plate shock has been observed experimentally. The computational results confirm the oscillatory feature in several kHz. Unsteady calculation with algebraic turbulence model is also performed. It is found that the laminar and turbulent results have some discrepancy in the transient period. However, both of them reveal the oscillatory behavior with similar frequency.

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움직이는 평면으로의 충돌 제트에 대한 수치해석 (NUMERICAL ANALYSIS OF JET IMPINGING ON A MOVING PLATE)

  • 강수진;서석원;이관수
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.129-134
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    • 2011
  • In this paper, the confined single slot jet impingement is investigated numerically. Although the geometry of the jet impingement is simple, the flow pattern of the jet impingement is complex and the numerical results of the jet impingement is affected much by numerical methods. The first goal of this study is to analyze the effects of Reynolds models and numerical spatial discretization schemes on the results of heat transfer performance and the flaw characteristics and to select the best method. Various versions of the low Reynolds number k-epsilon turbulence models are compared. Using the selected numerical method, the flow field and heat transfer characteristics of confined single slot jet impingement on a moving plate are analyzed.

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에멀젼연료 충돌분무의 거동특성에 관한 연구 (Study of Behavior Characteristics of Impinging Spray of Emulsified Fuel)

  • 염정국;김학민
    • 대한기계학회논문집A
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    • 제39권9호
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    • pp.909-916
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    • 2015
  • 본 연구는 디젤-과산화수소 에멀젼연료의 충돌분무를 대상으로 과산화수소의 혼합비가 증발분무 거동특성에 미치는 영향을 조사하였다. 에멀젼연료의 증발을 위해 온도조절이 가능한 가열판을 사용하여 온도를 $150^{\circ}C$, $200^{\circ}C$$250^{\circ}C$로 각각 설정하였고, 연료 분사압력을 400bar, 600bar, 800bar 및 1000bar로 설정하여 분사압력이 에멀젼연료의 증발특성에 미치는 영향을 확인하였다. 에멀젼연료의 혼합을 위 한 계면활성제로 span80과 tween80을 9:1의 비율로 혼합하여 에멀젼연료 전체 체적의 3%로 고정하였고 과산화수소의 혼합비율을 EF(Emulsified Fuel)0, EF2, EF12 및 EF22로 설정하여 디젤연료와 혼합하였다. 또한 에멀젼연료 증발 충돌분무의 가시화를 위해 슐리렌방법을 적용하였다. 본 연구의 결과로서 충돌하는 가열판의 온도와 분사압력이 높을수록 에멀젼연료 증발 촉진으로 연료 기상의 확산이 활발해지는 것을 알 수 있었다. 이러한 결과로부터 실제엔진에 에멀젼연료를 사용할 경우 연료 내 과산화수소 증발에 의한 연소실 온도 저하효과와 함께 보다 신속한 혼합기 형성은 엔진배출물의 감소를 일으키는 것으로 기대된다.

A study on the simulation of water cooling process for the prediction of plate deformation due to line heating

  • Nomoto, Toshiharu;Jang, Chang-Doo;Ha, Yun-Sok;Lee, Hae-Woo;Ko, Dae-Eun
    • International Journal of Ocean System Engineering
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    • 제1권1호
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    • pp.46-51
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    • 2011
  • In a line heating process for hull forming, the phase of the steel transforms from austenite to martensite, bainite, ferrite, or pearlite depending on the actual speed of cooling following line heating. In order to simulate the water cooling process widely used in shipyards, a heat transfer analysis on the effects of impinging water jet, film boiling, and radiation was performed. From the above simulation it was possible to obtain the actual speed of cooling and volume percentage of each phase in the inherent strain region of a line heated steel plate. Based on the material properties calculated from the volume percentage of each phase, it should be possible to predict the plate deformations due to line heating with better precision. Compared to the line heating experimental results, the simulated water cooling process method was verified to improve the predictability of the plate deformation due to line heating.

고속 원형충돌제트의 불안정 특성 (2) (Instabilities of High-speed Impinging Circular Jets(2))

  • 임정빈;김현중;권영필
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1998년도 춘계학술대회논문집; 용평리조트 타워콘도, 21-22 May 1998
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    • pp.486-491
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    • 1998
  • 본 연구에서는 충돌면의 형상에 따른 고속 원형 충돌제트의 불안정 모드를 밝히기 위하여 우선 충돌면의 형상에 따른 주파수 특성을 비교하고자 하였다. 이를 위해 충돌면이 제트의 직경보다 작은 원판(small plate)과 제트의 직경보다 큰 구멍(hole)의 2가지 경우에 대하여 실험을 하였고, 평판 충돌음에 대한 연구결과와 비교 검토하였다.

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수직평판에 충돌하는 초음속, 이중, 동축 제트유동에 관한 실험적 연구 (Experimental Study of the Supersonic Dual, Coaxial Jet Impinging on a Flat Plate)

  • 김중배;이준희;우선훈;이장창;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2002년도 제18회 학술발표대회 논문초록집
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    • pp.44-45
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    • 2002
  • 일반적으로 노즐이나 오리피스로부터 방출되는 초음속 단일 자유제트 유동의 경우, 제트내부에서 발생하는 충격파 시스템이나, 제트경계의 형상 그리고 제트코어의 길이 및 초음속 영역의 길이 등은 종래의 연구로부터 비교적 잘 알려져 있다. 이들 연구에 의하면, 제트의 압력비가 어느 정도 증가하게 되면, 노즐 하류에서 제트내부에는 마하 디스크가 발생하게 되며, 제트유동은 압축과 팽창을 반복하는 구조로 된다. 또 노즐 출구로부터 마하 디스크까지의 거리와 마하 디스크의 직경 등은 노즐의 압력비의 함수로 주어진다고 알려져 있다.

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유동가속부식으로 인한 급수가열기 동체 감육현상 규명과 완화 방안 및 충격판 설계개선에 관한 연구 (A Study on the Shell Wall Thinning by Flow Acceleration Corrosion and Mitigation Plan and Design Modification of a Feedwater Heater Impingement Baffle)

  • 김경훈;황경모;김인태
    • 한국분무공학회지
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    • 제15권2호
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    • pp.83-93
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    • 2010
  • Feedwater heaters of many nuclear power plants have recently experienced severe wall thinning damage, which will increase as operating time progresses. Several nuclear power plants in Korea have experienced wall thinning damage in the area around the impingement baffle inside feedwater heater installed downstream of the turbine extraction stream line. At that point, the extract steam from the turbine is two phase fluid at high temperature, high pressure, and high speed. Since it flows to reverse direction after impinging the impingement baffle, the shell wall of feedwater heaters may be affected by flow-accelerated corrosion. In this paper, to compare degree of shell wall thinning mitigation rate to squared type with mitigation rate of other type baffle plate, four different types of impingement baffle plate-squared, curved, mitigating type and multi-hole type-applied inside the shell. With these comparison data, this paper describes operation of experiments and numerical analysis which is composed similar condition with real feed water heater. And flow visualization is operated for verification of experiments and numerical analysis. In conclusion, this study shows that mitigating type and multi-hole type baffle plate are more effective than other baffle plate about prevention of pressure concentration and pressure value decrease.