• Title/Summary/Keyword: visualization test

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Development of X-ray Micro Computed Tomography and Applications (미세 X선 단층촬영 기법의 개발과 적용)

  • Kim, Seung-Gon;Lim, Jae-Hong;Kim, Bo-Heum;Lee, Eui-Jae;Lee, Sang-Joon
    • Journal of the Korean Society of Visualization
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    • v.8 no.2
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    • pp.45-50
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    • 2010
  • The objective of this study is to elucidate the feasibility of synchrotron X-ray micro CT as a non-destructive imaging method to visualize the three-dimensional morphological structures of biological and non-biological samples. The experiments were conducted in 7B2 X-ray micro CT beamline in Pohang Accelerate Laboratory (PAL). A rotational 3-axis stage was specially designed for $0^{\circ}-180^{\circ}$ scanning of test samples. Preliminary tests were performed for opaque samples including a mosquito head, a plant seed and gas diffusion layer (GDL) of polymer electrolyte fuel cell to verify the feasibility of the X-ray micro CT. It visualized clearly the internal structure of all the test samples, supporting its usefulness.

A Study on the Lubricating Air-layer Detection Techniques with Digital Image Analysis in Flat Plate Air Lubrication Test (공기윤활평판실험에서 디지털 영상분석을 통한 윤활공기막 검출기법)

  • Park, SeongHyeon;Lee, Inwon
    • Journal of the Korean Society of Visualization
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    • v.14 no.1
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    • pp.27-32
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    • 2016
  • The reduction of $CO_2$ emissions has been a key target in the Marine Industry since the IMO's Marine Environment Protection Committee published its findings in 2009. The representative emission index is termed as the EEDI (Energy Efficiency Design Index) for the new ships. Among various flow control techniques ever proposed, the air lubrication method is the one of most promising one in terms of practical applicability. The present study examines the basic characteristics of the flat plate test with intention of applying the air lubrication technology to the reduction of the resistance of a ship. Image analysis technique is proposed as a tool to quantify the effectiveness of the air lubrication method.

Development of a Recursive Local-Correlation PIV Algorithm and Its Performance Test

  • Daichin Daichin;Lee Sang Joon
    • 한국가시화정보학회:학술대회논문집
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    • 2001.12a
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    • pp.75-85
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    • 2001
  • The hierarchic recursive local-correlation PIV algorithm with CBC(correlation based correction) method was developed to increase the spatial resolution of PIV results and to reduce error vectors. This new algorithm was applied to the single-frame and double-frame cross-correlation PIV techniques. In order to evaluate its performance, the recursive algorithm was tested using synthetic images, PIV standard images from Visualization Society of Japan, real flows including ventilation flow inside a vehicle passenger compartment and wake behind a circular cylinder with rib let surface. As a result, most spurious vectors were suppressed by employing CBC method. In addition, the hierarchical recursive correlation algorithm improved largely the sub-pixel accuracy of PIV results by decreasing the interrogation window size, increasing spatial resolution significantly.

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A Study on the Steady Intake Flow Characteristics of the Intake 3-Valve Cylinder Head (흡기3밸브 실린더 헤드의 흡입 정상유동 특성에 관한 연구)

  • Chung, Jae-Woo;Lee, Ki-Hyung;Kim, Woo-Tae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.24 no.6
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    • pp.880-885
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    • 2000
  • Flow patterns and steady flow characteristics of an intake 3valve cylinder head are not obviously declared. Thus, in the study, the characteristics and limitation of intake flow coefficient which applied to multi intake valve engine are introduced. The flow coefficient and tumble characteristics are investigated by means of the steady flow test and flow visualization method. As the results, it is found that the intake flow rate is dominated by effective valve open area. In addition, this paper shows that the mass flow rate of intake 3valve engine is greater than that of intake 2valve engine and tumble flow of intake 3valve engine is superior to that of intake 2valve engine.

The Numerical Study of Flow through Complicated-Channel with the Lattice Boltzmann Equation Method (Lattice Boltzmann Equation 방법을 복잡한 형상의 채널 유동 해석에 적용하기 위한 수치적 연구)

  • Jeong Gl-Ho;Ha Man-Young
    • Journal of the Korean Society of Visualization
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    • v.2 no.1
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    • pp.46-51
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    • 2004
  • This paper deals with the evaluation of several boundary conditions which are commonly used in the lattice Boltzmann equation method. 2-D channel flow(Poiseuille flow) and lid-driven cavity flow was selected as a test problem of this study, because there exist an analytic solution and previous study which could be used for a benchmarking test. It was found that lattice Boltzmann method still needs more considerations of stability and physical consistency, though it could predict the flow patterns both qualitatively and quantitatively.

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An Experimental Study on Engine Cooling System Improvement (엔진 냉각 시스템 개선에 관한 실험적 연구)

  • Chon, M.S.;Hwang, Y.H.
    • Journal of ILASS-Korea
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    • v.9 no.4
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    • pp.77-82
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    • 2004
  • This paper describes the improvement of engine cooling system. To improve engine cooling performance, the authors approached in two ways. One is to increase water pump performance, changing of impeller shape and lightening of material were carried out. The second one is cooling efficiency rise, which were investigated with head gasket coolant flow passage optimization with flow visualization technique. The test results show that water pump performance was increased effectively, reduction of pump drive torque, and increase of pump flow-rate and pressure rise. Gasket hole pattern optimization test results represent an optimized head coolant flow which stands cross flow from exhaust to intake port side and small vortex were removed.

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A Study on the Characteristics of Air flow Fields with Velocity Uniformity in a Wind Tunnel (풍동장치 내 공기 유동장과 속도 균일도 특성에 대한 분석)

  • Han, Seok Jong;Lee, Sang Ho;Lee, Jae Gyu
    • Journal of the Korean Society of Visualization
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    • v.16 no.3
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    • pp.59-64
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    • 2018
  • Numerical simulations were carried out to analyze the flow characteristics of the wind tunnel. Flow field characteristics with velocity uniformity at the test sections are largely affected by inlet conditions of air flow rate and temperature. Axial average velocity of the flow field inside the test area was almost linearly decreased by 0.026% each 1m. The uniformity distributions of axial velocity showed the highest reduction rate of about 24% between nozzle outlets 1 ~ 2m. In addition, average velocity and the uniformity are increased with air temperature in the wind tunnel due to density variation. The results of this paper are expected to be useful for the basic design of wind tunnel and to be used for efficient design.

Development of National R&D Information Navigation System Based on Information Filtering and Visualization (정보 필터링과 시각화에 기반한 국가R&D정보 내비게이션 시스템 개발)

  • Lee, Byeong-Hee;Shon, Kang-Ryul
    • The Journal of the Korea Contents Association
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    • v.14 no.4
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    • pp.418-424
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    • 2014
  • This paper aim; to develop the National R&D Information Navigation System(NRnDINS) that is convenient and easy to use by the researchers on the basis of information filtering and visualization by converging and integrating the three types of the contents, namely, paper, report and project at the stage of development of the information system An information system is developed by establishing ontology and RDF on the three types of contents, and by applying information filtering and semantic search technology after having created the prototype for the screen by reflecting the user needs analysis and information visualization elements surveyed at the previous stage of information service planning. In this paper, to make the measure for information filtering, R&D navigation index is prosed and implemented, and NRnDINS capable of integrated search of the R&D contents through information visualization is developed. Also, for the testing of the developed system, the preference survey for its design by 1m persons and usability test of the system by 10 users are performed The result of the survey on the preference for the design is affirmative with 85% of the subjects finding it favorable and the composite receptivity is good with the score of 87.2 the results of the usability test. However, it was also found that further development of the personalization functions is needed. It is hoped that the R&D navigation index of the proposed and implemented in this paper would present quantitative objectivity and will induce further development of other information filtering index of contents in the future.

Study of the Wake Flow Around a Circular Cylinder (단독 원기둥 주위의 후류유동에 관한 연구)

  • Lee, Jaesung;Kim, Sangil;Seung, Samsun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.11
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    • pp.891-896
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    • 2015
  • This experimental study investigated the wake flow around an elastically supported circular cylinder. In this study, the Reynolds numbers are varied in the region of $1.4{\times}10^4{\leq}Re{\leq}3.2{\times}10^4$. Under these conditions, we have captured the process of the wake mechanism and the moving path of the vortex by measuring the velocity at each position in the wake around the cylinder. Further, these facts from the wind tunnel test are proved by a flow visualization test through a water channel. From the result, we have arrived at the following conclusions : i) The process (formation${\rightarrow}$growth${\rightarrow}$collapse) of vortex is observed in the wake around the cylinder, ii) The vortex efflux angle is approximately $16^{\circ}{\sim}17^{\circ}$ under the experimental conditions. These angles have no relationship with the velocity change and the existence of flow-induced vibrations of the cylinder, and iii) The moving path of the vortex center is obtained by spectrum analysis of the fluctuating velocity behind the cylinder. These are confirmed by conducting visualization tests.

Flmae Visualization of the sector combustor (분할연소기의 화염 가시화 연구)

  • Kim, Bo-Ra-Mi;Choi, Chea-Hong;Kim, Chun-Taek;Choi, Seong-Man
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.213-216
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    • 2009
  • In order to see the flame behavior in the gas turbine combustor, combustion test was performed by using sector combustor. Ignition test with torch ignition system was carried out at the various combustor inlet velocity and air fuel ratio. Also, flame blow out limit was measured by changing fuel flow rate with fixed air mass flow rate. In the test results, stable ignition is possible at air excess ratio of 6 and this limit is gradually increased with combustor inlet air velocity. The minimum blow out limit is about 4 at 40 m/s of combustor inlet velocity. This blow out limit is also increased up to about 10 with increasing combustor inlet velocity.

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