• Title/Summary/Keyword: PIV 계측기법

Search Result 62, Processing Time 0.028 seconds

NACA단면의 끝단 와방출에 대한 연구

  • Lee, Chang-U;O, U-Jun;Son, Chang-Bae;Kim, Ok-Seok;Lee, Gyeong-U
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
    • /
    • 2010.10a
    • /
    • pp.48-49
    • /
    • 2010
  • 선박의 러더하부 끝단에서는 선회에 따른 와류로 인하여 선회력 및 후류유동에 변화를 초래한다. 이를 관측하기 위해 NACA단면 형상의 몰수체를 영각과 관측단면을 변화시키며 $Re=2.0{\times}10^4$에서 실험을 통한 순간유동장을 계측 후 그 영향을 조사하였다. 계측된 결과는 상호상관 PIV기법을 이용 Naca단면 끝단에서의 2차원 유동특성을 알아보기 위하여 상호 비교하였다. NACA단면은 영각변화에 따라 후류유동에 영향을 미친다. 동일유입유속에서 영각이 증가함에 따라 관찰단면이 중앙으로 갈수록 와류 규모가 확대되는 것을 관찰할 수 있었다.

  • PDF

Development of high efficiency impeller for the process of ABS resin cohesion by using flow measurement (유동계측을 이용한 ABS 수지 응집 공정 혁신을 위한 고성능 교반기 임펠러 개발)

  • Kim, Jung-Hwan;Park, Jae-Hyoun;Lee, Hyun-Sik;Ok, Pyeong-Kweon;An, Ik-Jin
    • Proceedings of the Korean Society of Marine Engineers Conference
    • /
    • 2006.06a
    • /
    • pp.325-326
    • /
    • 2006
  • 현 화학플랜트에서 사용되고 있는 ABS 수지 응집 공정의 경우 교반기 내부의 불균일한 유동분포와 유동메커니즘의 문제점은 공정 제품의 생산성을 저하 시키는 원인으로 작용하고 있다. 그러나 우수한 성능의 산업용 교반기를 설계하기 위해선 반드시 교반성능에 영향을 미치는 다양한 내부의 유동특성의 정량적인 실험 데이터 확보가 필요하나, 3차원적 비정상 특성을 나타내는 복잡한 구조의 내부 유동특성에 관한 정량적 해석은 현재까지도 상당한 어려운 문제로 남아있다. 이에 이런 문제점을 개선하여 생산성을 향상시키기 위해서는 PIV 기법을 이용한 교반기 내부의 유동분포와 유동메커니즘을 규명하여 교반기 내부의 최적화된 유동을 형성시키는 임펠러의 형상을 개발하고자 한다.

  • PDF

Measurement of Honeycomb Turbulence in a Cavitation Tunnel Using Particle Image Velocimetry Method (PIV 기법을 이용한 캐비테이션 터널에서의 Honeycomb 난류 계측)

  • Ryu, Min-Cheol;Oh, Jung-Geun;Kim, Yoo-Chul;Koh, Won-Gyu;Lee, Youn-Mo;Suh, Jung-Chun
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.45 no.1
    • /
    • pp.42-53
    • /
    • 2008
  • The two dimensional PIV (particle image velocimetry) measurement technique is applied to water flow in a narrow cavitation tunnel. The nearly homogeneous and isotropic turbulent flows are generated by the honeycomb installed in the tunnel and visualized with a PIV technique. The velocities in the measurement plane at the tunnel centerline 184cm downward from the honeycomb were measured and calculated by an image correlation technique. The turbulent properties are evaluated and each term in the turbulent kinetic energy equation is calculated for the conditions with different internal pressures. Lowering the internal pressure gives an effect on the turbulent flow due to growing bubbles which are resolved in the water. The turbulent kinetic energy in the measurement plane is decayed much slower than those of other research results carried out with wind tunnels. With decreasing the tunnel internal pressures the turbulent intensities are increased about 1.5 times and the anisotropic tendency is also increased.

An Experimental Study on the Flow Characteristics around Wedge Type Structure by Slamming (슬래밍에 의한 쐐기형 구조물 주위의 유동특성에 관한 실험적 연구)

  • Oh, Seung-Jin;Cho, Dae-Hwan
    • Journal of the Korean Society of Marine Environment & Safety
    • /
    • v.19 no.2
    • /
    • pp.213-218
    • /
    • 2013
  • This paper presents are experimental investigation to figure out slamming impact pressure and flow characteristics of a wedge type structure in free fall. The flow field has been obtained by 2-frame grey level cross correlation PIV(Particle Image Velocimetry) method, the impact presure of free fall structure by a pressure acquisition system apply to Dewetron system. The angles between a model and the free surface are adapted $15^{\circ}$, $25^{\circ}$, $35^{\circ}$ and $45^{\circ}$ respectively. Velocity field of water exit has higher better than water entry. The impact pressure under the bottom of the model ha been appeared higher values at 15 degrees than 45 degrees, and also at P1.

An Experimental Study on Slamming Impact Pressure and Flow Characteristics by Free Fall of Rectangular Marine Structure (직사각형 해양구조물의 자유낙하 슬래밍 충격압력 및 유동특성에 관한 실험적 연구)

  • Oh, Seung-Jin;Gim, Ok-Sok;Lee, Gyoung-Woo;Cho, Dae-Wan
    • Journal of the Korean Society of Marine Environment & Safety
    • /
    • v.18 no.4
    • /
    • pp.371-377
    • /
    • 2012
  • This paper presents an experimental investigation to figure out slamming impact pressure and flow characteristics of a rectangular Marine structure($800{\times}250{\times}50mm^3$) in free fall. The flow field has been obtained by 2-frame grey level cross correlation PIV(Particle Image Velocimetry) method, the impact pressure of the free fall model by a pressure acquisition system(Dewatron). The angles between a model and the free surface are adapted $10^{\circ}$ and $20^{\circ}$ respectively. Velocity field of water exit has higher better than water entry. The highest point, P2 of impact pressure under the bottom of the model has been appeared about 6 % higher values at 20 degrees than 10 degrees.

Numerical Analysis on the Pressure Distributions around a Circular Cylinder by Control Rods (제어봉에 의한 원형실린더 주위의 압력분포에 관한 수치해석)

  • Gim, Ok-Sok;Lee, Gyoung-Woo;Cho, Dae-Hwan
    • Journal of Navigation and Port Research
    • /
    • v.31 no.6
    • /
    • pp.485-490
    • /
    • 2007
  • The purpose in having a control rod on a buoy system is to control the motion of it. The system may be composed entirely of a single circular cylinder and a long mooring anchor cable. A control rod has one function to perform in meeting its purpose, and that is to develop a control force in consequence of its orientation and movement relative to the water. The forces and moments generated as a result of the effects of mutual interference. then determine the stability characteristics of the body. In this paper, the study of control-rod-attached buoy's 2-dimensional section was accomplished. model tests and numerical simulations had been carried out with different diameters of control rods. and varying the Reynolds number $Re=5,000{\sim}25,000$ based on the cylinder diameter(D=50mm) to predict the performance of the body and the 2 frame particle tracking method Iud been used to obtain the velocity distribution in the flow field. 50mm circular cylinder Iud been used during the whole experiments and measured results had been compared with each other.

Turbulent Flow over 2-D Rectangular-Shaped Roughness Elements with Various Spacings(Part 1 : Time Averaged Flow) (사각단면을 갖는 환경 거칠기 요소의 거칠기 간격에 따른 유동 변화 (제1보: 평균유동장))

  • Hyun B.S.;Suh E.J.;Kim M.R.;Choi K.C.
    • Journal of the Korean Society for Marine Environment & Energy
    • /
    • v.9 no.2
    • /
    • pp.79-84
    • /
    • 2006
  • The present study deals with the flow over a flat plate with repeated roughness elements of 2-dimensional rectangular shape, which can be applied into the study on the natural geographical roughness and the turbulent flow on roughened solid surface. Experiment was performed using PIV technique in the circulating water channel. Results showed that the flow over roughness elements was characterized by the high shear flow emanating from top of roughness element and the recirculating region formed at the trough of two roughness elements. In general, the ratio between the spacing and the height of roughness elements plays a crucial role in developing the flow pattern near wall surface.

  • PDF

Experimental Study of Flow Characteristics with Swirl Number on Dump Combustor (모형 가스터빈 연소기에서 스월수에 따른 유동 특성에 관한 실험적 연구)

  • Park, Jae-Young;Han, Dong-Sik;Kim, Han-Seok;Song, Ju-Hun;Chang, Young-June;Jeon, Chung-Hwan
    • Journal of Energy Engineering
    • /
    • v.20 no.4
    • /
    • pp.338-345
    • /
    • 2011
  • The swirl flow applied for high efficiency and reduction of emission such as NOx, CO in a gas turbine engine makes recirculation zone by shear layer in the combustion chamber. This recirculation zone influences a decreasing flame temperature and flame length by burned gas recirculation. Also it is able to suppress from instability in lean-premixed flame. In this study, it was found that the swirl flow field was characterized as function of swirl number using PIV measurement in dump combustor. As increasing swirl number, a change of flow field was presented and recirculation zone was shifted in the nozzle exit direction. Also turbulent intensity and turbulent length scale in combustor were decreased in combustion. It has shown reduction of eddies scale with swirl number increasing.

Control Effects of the Hydrodynamic Force of the Submerged NACA0018 arranging in a Row in a Uniform Stream (균일흐름 중에 놓인 병렬구조를 가진 몰수형 NACA0018의 간격변화가 유체력 제어효과에 미치는 영향)

  • Gim, Ok-Sok;Shon, Chang-Bae;Lee, Gyoung-Woo
    • Journal of Navigation and Port Research
    • /
    • v.34 no.5
    • /
    • pp.325-330
    • /
    • 2010
  • An open water rudder test was carried out to figure out the flow characteristics around a twin rudder at $Re=1.5{\times}10^4$. In the analysis, the unique characteristics of a twin rudder, which affects rudder forces, were explained. The analysis includes varying angles of attack from 10 to 30 degrees. In this paper, the measured results have been compared with each other to predict the performance characteristics of a twin rudder's 2-dimensional section by 2-frame grey level cross correlation PIV method. The length L=0.75C between upper and lower rudders could be defined as the critical length.

Flow control on the near wake of a circular cylinder attached with control rods (제어봉 부착에 따른 원형실린더 근접 후류 유동제어에 관한 실험적 연구)

  • Gim, Ok-Sok;Lee, Gyoung-Woo
    • Journal of Navigation and Port Research
    • /
    • v.32 no.6
    • /
    • pp.453-458
    • /
    • 2008
  • Flow characteristics of the control-rod-attached 2-dimensional circular cylinder was accomplished using by PIV techniques. model tests had been carried out with different diameters of control rods(d/D=0.1 through d/D=0.5). and the Reynolds number Re=15,000 based on the cylinder diameter(D=50mm) to predict the performance of the model and the two-frame grey-level cross-correlation method had been used to obtain the velocity distribution in the flow field. 50mm circular cylinder had been used during the whole experiments and measured results had been compared with each other. The measured results have been compared with each case. therefore this article identifies not only the mean velocity profiles but also the control effects of the control rods.