• Title/Summary/Keyword: flat-plate

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Experimental Study on Fuel-Air Mixing Using Flat Plate/Cavity in Supersonic Flow (초음속 유동장 내 평판/cavity를 이용한 연료-공기 혼합의 실험적 연구)

  • Kim, Jeong-Woo;Jeong, Eun-Ju;Kim, Chae-Hyoung;Jeung, In-Seuck
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.319-322
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    • 2006
  • Rapid mixing of air-fuel (<1 ms) is needed to accomplish supersonic combustion. In this experiment, helium was injected laterally in to the Mach 1.92 air flow. 2 kinds of model, flat plate/cavity, were used in this experiment and images were taken by schlieren visualization. Pressure was affected by shock structure in the supersonic duct, and penetration height was increased by increasing J. Penetration height was higher in the cavity model than flat plate model.

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Development of 8-node Flat Shell Element for the Analysis of Folded Plate Structures (절판 구조물의 해석을 위한 8절점 평면 첼 요소의 개발)

  • 최창근;한인선
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 1999.04a
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    • pp.234-241
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    • 1999
  • In this study, an improved 8-node flat shell element is presented for the analysis of shell structure, by combining 8-node membrane element with drilling degree-of-freedom and 8-node plate bending element based on the recently presented technique. Firstly, 8-node membrane element designated as CLM8 is presented in this paper. The element has drilling degree-of.freedom in addition to transitional degree-of-freedom. Therefore the element possesses 3 degrees-of-freedom per each node which as well as the improvement of the element behavior, permits an easy connection to other element with rotational degree-of -freedom. Secondly. 8-node flat shell element was composed by adding 8-node Mindlin plate bending element to the membrane element. The behavior of the introduced plate bending element is further improved by combined use of nonconforming displacement modes, selectively reduced integration scheme and assumed shear strain fields. The element passes in the patch test, doesn't show spurious mechanism and doesn't produce shear locking phenomena. Finally, Numerical examples are presented to show the performance of flat shell element developed in the present study.

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Improvement of Shear Performance for High Ductile Fiber-Reinforced Mortar Slab-Column Connection in Flat Plate Structural System (고인성 복합섬유 모르타르를 이용한 플랫 플레이트 구조 슬래브-기둥 접합부의 전단성능 개선)

  • Ha Gee Joo;Kim Yun Yong;Shin Jong Hak;Yang Seung Hyeok;Hong Kun Ho;Kim Joung Su
    • Proceedings of the Korea Concrete Institute Conference
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    • 2005.11a
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    • pp.145-148
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    • 2005
  • Recently the construction of high-rise reinforced concrete building is progressively increased as the social demands. It is significantly important factors such as economy, the safety of structure, and the flexibility of internal space. Therefore new structural system is also required to be attained the reduction of story height, the flexibility and efficient use of space. The most suitable structural system is with the economy and flexibility, flat plate slab system in high-rise reinforced concrete building. In this research, it was focused in the improvement of shear performance in the flat plate system using high ductile fiber reinforced mortar. It was evaluated the shear performance in the critical region of slab-column connection. The flat plate system, designed by the high performance and safety, was developed as a new technique in the application of high-rise R/C building.

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Shear Reinforcement for Flat Plate-Column Connections using Lattice Bars (래티스형 철근을 이용한 무량판 구조의 접합부 전단보강)

  • 안경수;박홍근
    • Proceedings of the Korea Concrete Institute Conference
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    • 2003.11a
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    • pp.587-590
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    • 2003
  • In flat-plate floors, slab-column connections are broken down with a brittle shear failure. And it can cause the collapse of the whole structures. Thus, the proper method of shear reinforcement in flat plate-column connections must be required. The objective of this study is to compare shear reinforcement specimens using lattice bars to no shear reinforcement specimens in view of shear strength and ductility of the flat plate-column connections. The test results have shown that shear reinforcement specimens varying $\rho$, $b_0$/d and $C_1$/$C_2$ increase in shear strength by 36.85% and in ductility by 9.16 for no shear reinforcement specimens on the average. This results confirm the effectiveness of this type of shear reinforcement in improving shear strength and ductility.

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Experimental Study on the Structural Behaviors of Reinforced Flat Plate Under Lateral Loads (수평하중하에서 철근 콘크리트 플랫 플레이트의 구조적 거동에 관한 실험적 연구)

  • 조영직;박성무
    • Proceedings of the Korea Concrete Institute Conference
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    • 1995.10a
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    • pp.323-328
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    • 1995
  • This paper is experimental study to define the structural behaviors of reinforced flat plate under combined gravity and lateral loads. Specific objectives of this study reported herein are : (1) To study the behavior of a typical slab-column subassemblage under lateral loading. (2) To study the effects of vertical loads on slab-column lateral load behavior. (3) To investigate the post-failure behavior of slab-column connetios. To achieve these objectives, this study includes four tests of slab-column subassemblages that were made for 1/2 scale. Finally, Test results of this study show that the level of gravity load on the flat plate is one of the most important factors determining the lateral behavior of flat plate connections.

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The Characteristic of Friction-Factor on Honeycomb Surfaces (Part I : Experimantal Tests and Friction-Factor Modeling) (허니콤 표면의 마찰계수 특성에 관한 연구 (Part 1 : 표면 마찰계수 측정 및 모델링))

  • 하태웅
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.6
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    • pp.1430-1438
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    • 1994
  • Friction-factors for honeycomb surfaces are measured with a flat plate tester. The flat plate test apparatus is described and method is discussed for determining the friction-factor experimentally. The friction-factor is calculated for the flat plate test based on the Fanno-line flow. The test parameters are honeycomb cell width, depth, clearance, inlet pressure, and Reynolds number(or Mach number). A new empirical friction-factor model for honeycomb surfaces are developed as a function of these parameters.

A Study on the Heat Transfer from a Flat Plate and the Heat Transfer Enhancement by the Vortex Generator (평판에서의 열전달 및 와류발생기에 의한 열전달 촉진에 관한 연구)

  • Yoo, Seong-Yeon;Song, Si-Young;Park, Jong-Hark
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.1447-1452
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    • 2003
  • Vortex is very interesting flow phenomena on the heat transfer enhancement. In the present study, naphthalene sublimation technique is used to determine the average and local mass transfer coefficients on the flat plate with vortex generator. A parametric study with Reynolds number and angle of attack is carried out to investigate the heat transfer enhancement. The heat transfer coefficients on the flat plate with rectangular type and delta type vortex generator are compared with those of the flat plate without the vortex generator. Comparing heat transfer coefficients between rectangular type and delta type vortex generator, rectangular type vortex generator has much higher value than delta type vortex generator at the same condition.

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Numerical Study on Shock-Vortex Interaction Behind a Flat Plate (평판 뒤 전단층에서의 충격파-와동 상호 간섭에 대한 수치적 연구)

  • Chang Se-Myong;Chang Keun-Shik
    • 한국전산유체공학회:학술대회논문집
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    • 1999.11a
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    • pp.23-28
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    • 1999
  • In this paper we study numerically the shock-vortex interaction in the shear layer generated by moving shock waves above and below a flat plate. The faster normal shock is diffracted at the tip of the flat plate, producing a starting vortex. The slower normal shock below the flat plate arrives soon later to run across the vortex and make interaction. The two shocks are merged together and reflected back at the closed end of the shock tube to impinge on the shear layer developing multiple vortexlets. The computational simulation based on Euler and Navier-Stokes equations shows good prediction.

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Unsteady Aerodynamics of Flat Plate with Porous Trailing-edge (다공성 표면 평판 끝 단 위의 비정상 공력 특성에 대한 연구)

  • Jeong, Ye-Eun;Moon, Young-J.
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03b
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    • pp.134-137
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    • 2008
  • In this study, a computational analysis is conducted to investigate the effects of porous surfaces on the lift and drag forces of the flat plate. With the porous treatment, it is found that the strength of the Karman vortex as well as its influences over the trailing-edge surface are much weakened, resulting in significant reduction of the pressure fluctuations over the flat plate. The drag and lift coefficients are decreased by 85% and 18%, respectively, compared to the solid surface. The computed results also indicate that the size of the porous surface area does not have much influences but the back side of the flat plate has non-negligible effects on the interaction between the wall and the Karman vortex. As a result, the lift coefficient for the solid back side case is decreased only by 50.5% compared to the solid case and the drag coefficient is even increased by 65%.

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A Study on Heat Transfer Enhancement from Flat Plate Using Multiple Tripping Wires (복수 트리핑 와이어를 사용한 평판에서의 열전달 촉진에 관한 연구)

  • Yoo, Seong-Yeon;Cho, Woong-Sun;Ahn, Jong-Kyu
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.24 no.12
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    • pp.837-845
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    • 2012
  • The purpose of this research is to investigate the heat transfer enhancement by the multiple tripping wires installed on a flat plate. Naphthalene sublimation technique is used to measure the local mass transfer coefficients, and then heat transfer coefficients are calculated using heat/mass transfer analogy. Experiments are performed for the developed and developing flow conditions. Local and average heat transfer coefficients from the flat plate with three tripping wires are compared with those of no and one tripping wire. Remarkable heat transfer enhancements are found resulting from the boundary layer separation by the tripping wires, especially in the laminar boundary layer.