• 제목/요약/키워드: Axial velocity

검색결과 751건 처리시간 0.024초

Dynamic elastic local buckling of piles under impact loads

  • Yang, J.;Ye, J.Q.
    • Structural Engineering and Mechanics
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    • 제13권5호
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    • pp.543-556
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    • 2002
  • A dynamic elastic local buckling analysis is presented for a pile subjected to an axial impact load. The pile is assumed to be geometrically perfect. The interactions between the pile and the surrounding soil are taken into account. The interactions include the normal pressure and skin friction on the surface of the pile due to the resistance of the soil. The analysis also includes the influence of the propagation of stress waves through the length of the pile to the distance at which buckling is initiated and the mass of the pile. A perturbation technique is used to determine the critical buckling length and the associated critical time. As a special case, the explicit expression for the buckling length of a pile is obtained without considering soil resistance and compared with the one obtained for a column by means of an alternative method. Numerical results obtained show good agreement with the experimental results. The effects of the normal pressure and the skin friction due to the surrounding soil, self-weight, stiffness and geometric dimension of the cross section on the critical buckling length are discussed. The sudden change of buckling modes is further considered to show the 'snap-through' phenomenon occurring as a result of stress wave propagation.

고층 아파트에서 응축기 적층문제 분석 (Analysis of the Condenser Stack Effect in a High-Rise Apartment Building)

  • 최석호;이관수;김인규;이동혁
    • 설비공학논문집
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    • 제16권9호
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    • pp.796-803
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    • 2004
  • The stack effect of a new type condenser installed in a high-rise apartment building was studied numerically A sirocco fan is introduced to the new type condenser instead of an axial flow In. The new type condenser intakes the cold air through the lower inlet and exhausts the hot air through the upper outlet. The effects of the building height and frontal wind on the performance of an air-conditioner were analyzed. The performance of an air-conditioner was evaluated by using COP (coefficient of performance) and CGPI (condenser group performance indicator). the hot air was exhausted by the new type condenser at an angle of 50$^{\circ}$ from the outer wall of the building. If there was no draft, the new type condenser installed in the high-rise apartment building had a good performance and its performance on each floor is not influenced by the stack effect. It is shown that the efficiency of the air-conditioner installed in several floors below the top floor decreased when the frontal wind velocity was greater than 8 m/s.

연료전지용 스크롤 공기압축기 개념설계 (Conceptual Design of the Scroll Air Compressor for Fuel Cell)

  • 권태훈;안종민;김현진;심재휘
    • 설비공학논문집
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    • 제20권2호
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    • pp.113-120
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    • 2008
  • Potential application of the scroll type machine to air compressor for fuel cell has been studied. Among the seven configuration factors which determine scroll wrap profile, the wrap thickness and the orbiting radius were chosen as two independent variables to generate various scroll wrap profiles. A conceptual design practice was conducted for scroll air compressor for SOFC with power output of 2 kW. With larger wrap thickness and orbiting radius, base plate area of the orbiting scroll becomes smaller, so is the axial gas force acting on the base plate, resulting in reduced thrust loss in spite of larger friction velocity. Performance analysis on the designed model showed that its total efficiency was 64.4% with the mass flow rate per unit compressor input of 0.00905 kg/(s kW) for the wrap thickness of 3.5 mm and the orbiting radius of 3.0 mm.

Fourier 급수전걔를 이용한 부분적으로 유체가 채워진 원통형 셸의 고유진동 해석 (Fourier Series Expansion Method for Free Vibration Analysis of a Partially Liquid-Filled Circular Cylindrical Shell)

  • 정경훈;이성철
    • 소음진동
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    • 제4권2호
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    • pp.163-175
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    • 1994
  • An analytical method for nautral frequencies of a partially liquid- filled circular cylindrical shell with various boundary conditions is developed by means of the Stokes's transformation and Fourier series expansion on the basis of Sanders' shell equation. The liquid-shell coupled system is divided into two regions for convenient formulation. One is the empty shell region in which the Sanders' shell equations are formulated without the lipuid effect, the other is wetted shell region in which the shell equations are formulated with consideration of the liquid dynamic effect. The shell equations for each regions are combined by the geometry and the force continuities at the junction of the two regions. For the vibration relevant to the liquid motion, the velocity potential of liquid is assumed as a sum of linear combination of suitable harmonic functions in axial direction. The unknown parameters are selected to satisfy the boundary condition along the wetted shell surface. The natural frequencies of the liquid filled cylindraical shells with the clamped- free and the clamped-clamped boundary conditions examined in the previous works, are obtained by this analytical method. The results are compared with the previous works, and excllent agreement is found for the natural frequencies of the shells.

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전기여과에 의한 거대이온성 분자체 분리현상연구 (Study on the separation of large ionic-molecules by electrofiltration)

  • 박영규
    • 전기화학회지
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    • 제1권1호
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    • pp.18-23
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    • 1998
  • 전기장이 충전층내 거대 이온성분자체의 분리를 위한 이론적 인 모델이 수행되었다 충전층내 여과재에서 전기적인 대류속도의 효과는 분자량이 큰 이온성 물질을 분리하기 위해서는 효과적이다. 이유는 전기장하에 거대이온성 분자체는 전기의 방향으로 빠르게 이온성분자체가 곧게 뻗는 현상때문이다. 이러한 분자체의 거동현상은 여과재내에 대류속도가 전기힘과 분자크기에 따라 대류속도가 다르기 나타나기 때문에 이들에 대한 연구는 충전층내에서 분자체를 분리하는데 도움이 된다 본 논문에서 여과재시스템내에서 이론분리는 확산에 대한 대류속도의 비$(Pe_t/Pe_g)$를 이용하여 예측하였으며 본 논문에서 얻어진 결과는 여과시스템을 설계하고 응용하는데 유효하게 적용될 것이며 이론적인 근거는 연산자 이론과 Reptation이론이 적용되였다.

Broadband Characterization of Circularly Polarized Waveguide Antennas Using L-Shaped Probe

  • Fukusako, Takeshi
    • Journal of electromagnetic engineering and science
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    • 제17권1호
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    • pp.1-8
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    • 2017
  • This paper introduces a technique to obtain the broadband characteristics of circularly polarized antennas using an L-shaped probe. A waveguide antenna is suitable for obtaining high gain and handling convenience in some applications; however, the asymmetrical structure of the L-shaped probe results in cross-polarization and frequency dependence on the field distribution of higher-order modes (HOM). In addition to the basic characteristics of a waveguide antenna with an L-shaped probe, the author discusses some techniques to reduce the HOM and cross-polarization. As a result, the 3-dB axial ratio (AR) is obtained with the fundamental mode even when the frequency is expanded to the region for HOM of TM. This reduction is mainly due to the cutoff structure to the TM mode around the short wall of the waveguide. Furthermore, some aperture modification techniques can reduce the cross-polarization in a wide range of angles in the radiation pattern. Such techniques and their mechanisms are discussed in this paper. The obtained performance shows that the proposed antennas have a wide range of angles of 3-dB AR in the radiation pattern, broadband characteristics in impedance and AR, and low variation in group velocity.

와동에 의해 교란된 대향류 비예혼합화염의 화학종 전달기구 및 화염구조 (Species Transport Mechanisnn and Flame Structure of Counterflow Nonpremixed Flame Perturbed by a Vortex)

  • 오창보;황철홍;이창언
    • 대한기계학회논문집B
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    • 제28권11호
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    • pp.1407-1416
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    • 2004
  • A two-dimensional direct numerical simulation was performed to investigate the flame structure of CH$_4$/$N_2$-Air counterflow nonpremixed flame interacting with a single vortex. The detailed transport properties and a modified 16-step augmented reduced mechanism based on Miller and Bowman's detailed chemistry were adopted in this computation. The results showed that an initially flat stagnation plane, on which an axial velocity was zero, was deformed into a complex-shaped plane, and an initial stagnation point was moved far away from a vortex head when the counterflow field was perturbed by the vortex. It was noted that the movement of stagnation point could alter the species transport mechanism to the flame surface. It was also identified that the altered species transport mechanism affected the distributions of the mixture fraction and the scalar dissipation rate.

Loss of Torque on Magnetic Fluid Seals with Rotating-shafts

  • Hu, Jianhui;Zhao, Meng;Wang, Lu;Zou, Jibin;Li, Yong
    • Journal of Magnetics
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    • 제22권2호
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    • pp.286-290
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    • 2017
  • The effects of loss of torque on magnetic fluid seals with rotating-shafts and the general difficulty of studying magnetic fluid seals are the focus of this work. The mechanism underlying loss of torque on such seals is analyzed using theoretical methods that show that loss of torque can be affected by several factors, including the velocity of the rotating-shaft, the structure of the sealing device, the characteristics of the magnetic field, and the characteristics of the magnetic fluid. In this paper, a model of the loss of torque is established, and the results of finite element analysis and testing and simulations are analyzed. It is concluded that (i) the viscosity of the magnetic fluid increased with the intensity of the magnetic field within a certain range; (ii) when the magnetic fluid was saturated, the increase in loss of torque tended to gradually slow down; and (iii) although the axial active length of the magnetic fluid may decrease with increasing speed of the rotating-shaft, the loss of torque increased because of increasing friction.

전단 자극 제어에 의한 동축 스월제트 수치 연구 (Numerical Study on Co-axial Swirl Jets by Shear Excitation Control)

  • 이원중
    • 항공우주기술
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    • 제12권1호
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    • pp.207-212
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    • 2013
  • 스월 제트 전단층 제어에 관한 인공적 방법의 가능성을 연구하기 위해 전단 자극장치가 제안되었다. 주요 구성품으로는 두개의 동심 아음속 노즐 그리고 유동 자극 생성을 위한 내부 돌기 등이다. 돌기의 숫자는 방위각 방향의 다양한 모드를 유도 할 수 있도록 변화가 가능하다. 획득된 속도 결과는 평면 contour plot과 공간 입자 궤적으로 표현하였다. 다양한 자극 모드에서의 결과 값들이 기준 값(무자극)과 비교되었다. 결과적으로, 새로 고안된 기법이 스월 유동 와류 구조 제어에 있어 효과적인 방법임이 입증되었다.

팬싱크의 유동 특성에 관한 실험 및 수치해석적 연구 (Experimental and Numerical Studies on the Flow Characteristics of a Fan-Sink)

  • 이경용;최영석;윤재호
    • 설비공학논문집
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    • 제18권3호
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    • pp.225-230
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    • 2006
  • The overall performance and local flow fields of the fan, heat sink, and fan-sink were experimentally and numerically studied to investigate the flow characteristics of a fan-sink. The flow resistance of the heat sink was measured by small fan tester based on AMCA standards and compared with the CFD results to select available cooling fan for the fan-sink. The nonuniform velocity profile behind the fan outlet was shown by the flow visualization. The effects of nonuniform velocities on the performance of heat sink were discussed. To validate the commercial CFD code CFX-5.6, the predicted performance curve was compared with that of fan testing. The local flow fields of the fan-sink were analyzed by CFD results. MFR (multiple frame of reference) was used as a computational model combining rotating fan and stationary heat sink. Through the CFD results of the fan-sink, the flow patterns behind the fan outlet influenced the flow resistance and overall performance of the heat sink.