• Title/Summary/Keyword: Air volume fraction

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Thermal behavior of the duct applied Functionally Graded Material (경사기능재료를 적용한 덕트의 열적거동해석)

  • Yoon, Dong-Young;Park, Jung-Sun;Im, Jong-Bin
    • Proceedings of the KSME Conference
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    • 2004.11a
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    • pp.516-521
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    • 2004
  • In unmanned aerial vehicles (UAV), the high temperature results from friction among the air, combustion of fuel in engine and combustion gas of a nozzle. The high temperature may cause serious damages in UAV structure. The Functionally Graded Material (FGM) is chosen as a material of thc engine duct structure. Thermal stress analysis of FGM is performed in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high temperature. Therefore, hoop stress, axial stress and shear stress of duct with 2 layers, 4 layers and 8 layers FGM are compared and analyzed respectively. In addition, the creep behavior of FGM used in duct structure of an engine is analyzed for better understanding of FGM characteristics.

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A Study on the Smoke Reduction of Methanol-Diesel Engine (메탄올-디젤기관의 스모크 저감에 관한 연구)

  • Han, Seong-Bin;Mun, Seong-Su
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.7
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    • pp.2421-2429
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    • 1996
  • The objective of this research is to apply effect of the pre-mixed combustion quantity and smoke emission in diesel engine. According as air fuel ratio is increased, emission of smoke concentration is linearly reduced. As Injection timing is advanced, smoke concentration is remarkably reduced. It is considered to be the primary cause of the increase in the premixed combustible mixture during long ignition delay period with advancing injection timing. Smoke is increased with increasing engine speed, so it is considered to be the primary cause of the increase of the mass of fuel injected. Smoke is decreased according to the increase of methanol volume ratio. It is considered that the primary cause of the increase in the quantity of pre-mixed combustion.

Multi-Step Reheating Process of Metal Matrix Composites for Thixoforming (Thixoforming을 위한 금속 복합재료의 다단 재가열 공정)

  • 허재찬;강충길
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1997.10a
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    • pp.180-183
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    • 1997
  • The forming process of metal matrix composites by the die casting and squeeze casting process are limited in size and dimension in term of final parts without machining. The thixoforming process for metal matrix composites has numerous advantages compared to die casting, squeeze casting and compocasting. The characteristics of thixoforming process can decrease the liquid segregation because of he improvement in fluidity in a globular microstructure state and utilizes flow without air entrapment. Therefore, in order to obtain the sound parts of metal matrix composites by using thixoforming process which as co-existing solidus-liquidus pahse, it si very important to obtain reheating condition. However, for he thixoforming process, the billet with the desired volume fraction must be heated to obtain a uniform temperature distribution over the entire cross-sectional areas. To obtain the reheating conditions of composites, the particulate reinforced metal matrix composites for thixoforming were fabricated by combined stirring process which is simultaneously performed with electro-magnetic stirring process which is simultaneously performed with electro-magnetic stirring and mechanical stirring process.

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NUMERICAL SIMULATION OF A TRANSONIC AIRFOIL IN THE CLOUD WITH THE DROPLET-LADEN INVISCID AIR FLOW MODEL (액적이 있는 비점성 공기유동 모델을 이용한 구름속의 천음속 에어포일 수치해석)

  • Yeom, G.S.;Chang, K.S.;Baek, S.W.
    • 한국전산유체공학회:학술대회논문집
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    • 2011.05a
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    • pp.291-293
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    • 2011
  • In this paper, the problem of transonic aerodynamic characteristics of a NACA0012 airfoil is numerically investigated in the inviscid gas-droplet two-phase flow with the compressible two-fluid model. In the present study, the airfoil flight in the cloud is simulated by taking account of the viscous drag of the droplets, the heat transfer, the phase change, and the droplet fragmentation The two-fluid equation system is solved by the fractional-step method and the WAF-HIL scheme. The effects of size and volume fraction of the droplets on the flow characteristics of the airfoil in the cloud are elaborated and discussed.

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THEORETICAL AND NUMERICAL STUDY ON SCAVENGE CHARACTERISTICS IN A SUBCHAMBER OP AN HCCI ENGINE (HCCI 엔진 부실내 소기특성에 대한 이론 및 수치해석적 연구)

  • Suh Y.K.;Heo H.S.
    • Journal of computational fluids engineering
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    • v.10 no.2
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    • pp.21-29
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    • 2005
  • In this paper, we present the theoretical and numerical results of scavenge characteristics in a small subchamber of an HCCI(Homogeneous Charge Compression Ignition) engine. Two theoretical models are proposed in prediction of the scavenge time and the efficiency; one is the non-mixing model in which the input gas(CH4) and the existing gas(air) do not mix at all, and the other is the fully-mixed model in which the two gases are assumed to mix completely before ejection. Focus is also given to the effect on the scavenge performance of the size of the chamber outlet.

Soot Formation and Oxidation of an Ethylene Laminar Diffusion Flame with Different Radiation Boundary Conditions (에틸렌 층류 확산화염의 복사경계조건에 따른 매연생성 및 산화특성)

  • Lee, Chun-Beom;Nam, Youn-Woo;Lee, Won-Nam;Shin, Hyun-Dong
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.11-18
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    • 2003
  • The soot formation and oxidation characteristics with different radiation boundary conditions have been studied experimentally in a co-flow ethylene/air laminar diffusion flame. The boundary conditions are two cases, one is a fully refractive radiation boundary condition by a polished aluminum cylinder(AL) and the other is a fully absorbing radiation boundary condition by a black body cylinder(BB). The AL case compared with BB condition show the lower inception point, denser soot volume fraction, wider and longer annular soot area owing to the reabsorption of radiating energy.

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Thermal Structural Analysis of a Duct with Heat Resistant Metal Materials for Smart UAV (고온 내열재료를 사용한 스마트 무인기 덕트의 열 구조 해석)

  • Im, J.B.;Yoon, D.Y.;Lee, K.M.;Park, J.S.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.12 no.2
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    • pp.17-28
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    • 2004
  • In unmanned aerial vehicle (UAV), the high temperature results from friction with the air, combustion of fuel and combustion gas of a nozzle etc. It causes serious problems in the UAV structure. The characteristic analysis of heat resistant metal and ceramic materials and creep analysis for the functionally graded material (FGM) is presented in this paper. FGM is composed of two constituent materials that are mixed up according to the specific volume fraction distribution in order to withstand high heat condition. In addition, the creep behavior of FGM applied in duct structure of an engine is analyzed.

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Natural Convection of Nanofluids Using Jang and Choi's Model for Effective Thermal Conductivity and Various Models for Effective Viscosity (Jang and Choi's Model과 다양한 점성계수 모텔을 이용한 나노유체에서의 자연대류 특성)

  • Hwang, Kyo-Sik;Jang, Seok-Pil
    • Proceedings of the SAREK Conference
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    • 2005.11a
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    • pp.539-545
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    • 2005
  • In this paper, the thermal characteristics of natural convection in a rectangular cavity with nanofluids such as water-based nanofluids containing alumina are theoretically investigated with a new model of the thermal conductivity for nanofluids presented by Jang and Choi and various models for effective viscosity. In addition, based on theoretical results, the effects of various parameters such as the volume fraction, the temperature, and the size of nanoparticles on free convective instability and heat transfer characteristics in a rectangular cavity with nanofluids are suggested.

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Fluid Flow Characteristics of $AL_2O_3$ Nanoparticles Suspended in Water (알루미나 나노유체의 유동 특성에 관한 연구)

  • Lee, Ji-Hwan;Jang, Seok-Pil
    • Proceedings of the SAREK Conference
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    • 2005.11a
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    • pp.546-551
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    • 2005
  • In this paper we report fluid flow characteristics of $AL_2O_3$ nanoparicles suspended in water. Especially, the effects of volume fraction with the range of 0.01% to 0.3% and inner diameter of tubes on the pressure drop and the effective viscosity of $AL_2O_3$ nanoparicles suspended in water are experimentally investigated. Experimental results are compared with analytic solution which can be derived with Einstein model. We confirm whether Einstein model which have been used to determine the effective viscosity of nanofluids is valid or not.

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A Study on the Radial Spray Performance of a Plaint-Jet Twin-Fluid Nozzle (액주형 이류체노즐의 반경반향 분무특성에 관한 연구)

  • 최진철;노병준;강신재
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.3
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    • pp.662-669
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    • 1994
  • In the combustion system, the optimum spray conditions reduce the pollutant emission of exhaust gas and enhance the fuel efficiency. The spray characteristics-the drop size, the drop velocity, the number density and the mass flux, become increasingly important in the design of combustor and in testifying numerical simulation of spray flow in the combustor. The purposes of this study are to clarify the spray characteristics of twin-fluid nozzle and to offer the data for combustor design and the numerical simulation of a spray flow. Spatial drop diameter was measured by immersion sampling method. The mean diameter, size distribution and uniformity of drop were analyzed with variations of air/liquid mass flow ratio. The results show that the SMD increases with the liquid supply flow rate and decreases with the air supply velocity. The radial distribution of SMD shows the larger drops can diffuse farther to the boundary of spray. And the drop size range is found to be wider close to the spray boundary where the maximum SMD locates.