• 제목/요약/키워드: constant area

검색결과 1,448건 처리시간 0.03초

Span 20과 Tween계 계면활성제의 물/공기 계면에서의 분자면적과 계면장력 거동 (Molecular Area and Interfacial Tension Behavior of Span 20 and Tween series surfactants at water/air interface)

  • 김천희
    • 한국의류학회지
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    • 제24권7호
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    • pp.1065-1072
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    • 2000
  • The molecular areas and the interfacial tension behavior of ten nonionic surfactants, i.e., Span 20 and Tween 20, 40, 60. 80, 21, 61, 81, 65, & 85 are tested to assay their effects on the wetting and liquid retention properties of hydrophilic and hydrophobic fibrous materials. The molecular areas at water/air interface are derived from Gibbs’adsorption equations. The following conclusions are drawn from the results: 1) Span 20 is efficient in lowering the interfacial tension and effective in adsorption at the water/air interface, resulting in the low interfacial tension at critical micelle concentration (${\gamma}$$_{CMC}$) and a small molecular area($\omega$), 2) when the hydrophiles of the surfactants are constant, $\omega$’s increase as hydrophobe carbon numbers of the surfactants increase, 3) when the hydrophobes are constant, ${\gamma}$$_{CMC}$’s and $\omega$’s increase as the hydrophile ethylene oxide units increase, indicating effectiveness and efficiency is parallel in this case, 4) the ethylene oxide unit length as a hydrophile has greater influence on u than the hydrophobe chain length.han the hydrophobe chain length.gth.

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Capacity Modulation of an Inverter Driven Heat Pump with Expansion Devices

  • Lee, Yong-Taek;Kim, Yong-Chan;Park, Youn-Cheol;Kim, Min-Soo
    • International Journal of Air-Conditioning and Refrigeration
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    • 제8권2호
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    • pp.60-68
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    • 2000
  • An experimental study was peformed to investigate characteristics of an inverter driven heat pump system with a variation of compressor frequency and expansion device. The compressor frequency varied from 30Hz to 75Hz, and the performance of the system ap-plying three different expansion devices such as capillary tube, thermostatic expansion valve(TXV), and electronic expansion valve (EEV) was measured. The load conditions were altered by varying the temperatures of the secondary fluid entering condenser and evaporator with a constant flow rate. When the test condition was deviated from the standard value(rated value), TXV and EEV showed better performance than capillary tube due to optimal control of mass flow rate and superheat. In the present study, it was observed that the variable area expansion device had better performance than constant area expansion device in the inverter heat pump system due to active control of flow area with a change of com-pressor frequency and load conditions.

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HEVC를 위한 저면적 고성능 다중 모드 1D 변환 블록 설계 (Low Area and High Performance Multi-mode 1D Transform Block Design for HEVC)

  • 김기현;류광기
    • 한국정보통신학회논문지
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    • 제18권1호
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    • pp.78-83
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    • 2014
  • 본 논문에서는 연산 시간이 긴 곱셈기 패스를 낮은 주파수에서 동작하는 저면적의 HEVC(High Efficiency Video Coding)용 다중 모드 일차원 변환 블록을 구현하는 효율적인 방법을 제시하였다. 제시한 방법은 전체 면적을 줄이기 위하여 일반적인 변수와 변수를 입력으로 받는 곱셈기 대신 행렬의 계수 특성을 이용한 상수와 변수를 입력으로 받는 상수 곱셈기를 사용하였다. 상수 곱셈기 사용으로 인하여 전체적인 처리량을 증가시켰으며 늘어난 처리량으로 인해 남는 동작 사이클을 이용하여 연산시간이 많이 걸리는 곱셈기 부분에 멀티 사이클 패스를 구성하여 곱셈기의 동작 주파수를 낮게 하면서 전체 연산량은 유지시켰다. TSMC 0.18um CMOS 공정 라이브러리를 이용하여 실제 하드웨어를 구현한 결과 4k($3840{\times}2160$) 영상을 기준으로 최소 동작 주파수는 186MHz이고 최대 동작 주파수는 300MHz이다.

RADICAL IGNITION TECHNIQUE IN A CONSTANT VOLUME CHAMBER

  • Park, J.S.;Ha, J.Y.;Yeom, J.K.;Lee, J.S.;Lee, C.J.;Chung, S.S.
    • International Journal of Automotive Technology
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    • 제8권3호
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    • pp.269-274
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    • 2007
  • A prior fundamental study was executed using a constant volume chamber (CVC) to improve the burning characteristics of lean pre-mixture by the injection of active radicals generated in the sub-chamber of the CVC. The Radical ignition (RI) technique shows remarkable progress in the burning velocity and combustible lean limit compared with the results of the spark ignition (SI) technique. The optimum design value of the sub-chamber geometry is near $0.11cm^{-1}$ for the ratio of the total area of the holes to the sub-chamber volume $(A_h/V_s)$. In this study, based on the former experimental results, the additional works have been performed to examine the effects of the geometry change in the number $(N_h)$, the total section area $(A_h)$, and diameter $(D_h)$ of the passage holes on the combustion characteristics in the CVC. Also ambient conditions such as the initial temperature and the initial pressure of the mixture were selected as experimental parameters and the effects of residual gas at the chamber on the combustion characteristics were investigated. As a result, the correlation between the passage hole number and overall passage hole area was grasped. The effects of the initial temperature were significant, but on the other hand, those of the initial pressure were weak. A more detailed analysis on the residual gas is required in the future.

초음속 동축제트의 유동특성에 관한 연구 (Study of the Flow Characteristics of Supersonic Coaxial Jets)

  • 이권희;구병수;김희동
    • 대한기계학회논문집B
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    • 제25권12호
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    • pp.1702-1710
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    • 2001
  • Supersonic coaxial jets are investigated numerically by using the axisymmetric, Wavier-Stokes equations which are solved using a fully implicit finite volume method. Three different kinds of coaxial nozzles are employed to understand the flow physics involved in the supersonic coaxial jets. Two convergent-divergent supersonic nozzles are designed to have the same Mach number 2.0, and used to compare the coaxial jet flows with those discharging from one constant-area nozzle. The impingement angle of the annular jets are varied. The primary pressure ratio is changed in the range from 2.0 to 10.0 and the assistant jet ratio from 1.0 to 3.0. The results obtained show that the fluctuations of the total pressure and Mach number along the jet axis are much higher in the constant-area nozzle than those in the convergent-divergent nozzles, and the constant-area nozzle lead to higher total pressure losses, compared with the convergent-divergent nozzles. The assistant jets from the annular nozzle affect the coaxial jet flows within the distance less than about ten times the nozzle throat diameter, but beyond it the coaxial jet is conical with self-similar velocity profiles. Increasing both the primary jet pressure ratio and the assistant jet pressure ratio produces a longer coaxial jet core.

도시 하수 폐기물의 고주파 건조 (Drying by Microwave Irradiation of Sewage Waste)

  • 박수인;박광하
    • 분석과학
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    • 제10권6호
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    • pp.418-426
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    • 1997
  • 고주파를 이용한 오니의 건조특성에 대하여 살펴보고 재래식 건조특성과 비교 분석하였다. 고주파 건조는 빠른 속도와 높은 효율을 보였다. 재래식 건조에서는 항율건조기간이 나타나지 않았고 수분은 모세관현상에 의하여 이동하였다. 오니의 수분 중 자유수와 결합수는 존재하지 않았다. 고주파 건조에서 감율건조기간이 두 부분으로 나타났으며, 수분의 이동은 확산에 의하여 일어났다. 증발 표면적이 커질수록 수분의 제거가 촉진되었고, 오니의 지름이 커질수록 넓은 범위의 항율건조 기간이 나타났으며, 모양에 따라서도 건조특성이 다르게 나타났다. 고주파 건조에서는 오니의 중심부에서 가장 먼저 온도가 상승하였으며, 항율건조기간에서 $80{\sim}100^{\circ}C$로 일정하게 유지되면서 가장 높았다.

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효율적인 4-2 Compressor와 보상 특성을 갖는 근사 곱셈기 (Approximate Multiplier With Efficient 4-2 Compressor and Compensation Characteristic)

  • 김석;서호성;김수;김대익
    • 한국전자통신학회논문지
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    • 제17권1호
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    • pp.173-180
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    • 2022
  • 근사 컴퓨팅은 효율적인 하드웨어 컴퓨팅 시스템을 설계하기 위한 유망한 방법이다. 근사 곱셈은 고성능, 저전력 컴퓨팅을 위한 근사 계산 방식에 사용되는 핵심적인 연산이다. 근사 4-2 compressor는 근사 곱셈을 위한 효율적인 하드웨어 회로를 구현할 수 있다. 본 논문에서는 저면적, 저전력 특성을 갖는 근사 곱셈기를 제안하였다. 근사 곱셈기 구조는 정확한 영역, 근사 영역, 상수 수정 영역의 세 영역으로 나누어진다. 새로운 4:2 근사 compressor를 사용하여 근사 영역의 부분 곱 축소를 단순화하고, 간단한 오류 수정 방식을 사용하여 근사로 인한 오류를 보상한다. 상수 수정 영역은 오차를 줄이기 위해 확률 분석을 통한 상수를 사용하였다. 8×8 곱셈기에 대한 실험 결과, 제안한 근사 곱셈기는 기존의 4-2 compressor 기반의 근사 곱셈기보다 적은 면적을 요구하면서 적은 전력을 소비함을 보였다.

정적연소기에서 라디칼 유도분사를 이용한 희박혼합기의 연소특성에 관한 연구 (2) (A Study on the Combustion Characteristics of Lean Mixture by Radicals Induced Injection in a Constant Volume Combustor (2))

  • 박종상;강병무;이명준;하종률;정성식
    • 한국자동차공학회논문집
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    • 제12권3호
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    • pp.19-26
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    • 2004
  • A prior fundamental study was executed using a constant volume chamber to improve the burning properties of lean pre-mixture by the injection of active radicals generated in the sub-chamber. In consequence, RI method shows remarkable progress in the aspects of burning velocity and combustible lean limit compared with SI method. In this study, the necessary additional works have been performed to be based on the former results. We changed parameters as the initial temperature and the initial pressure of mixture. And the effects of residual gas at issue in a real engine were investigated. As a result, the effects of initial temperature were significant, but on the other hand, those of initial pressure were slight. The correlation of passage hole number between overall passage hole area was grasped. And the more detailed analysis is required on residual gas.

이차원 Constant Geometry FFT VLSI 알고리즘 및 아키텍쳐 (VLSI Algorithms & Architectures for Two Dimensional Constant Geometry FFT)

  • 유재희;곽진석
    • 전자공학회논문지B
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    • 제31B권5호
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    • pp.12-25
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    • 1994
  • A two dimensional constant geometry FFT algorithms and architectures with shuffled inputs and normally ordered outputs are presented. It is suitable for VLSI implementation because all buterfly stages have identical, regular structure. Also a methodology using shuffled FFT inputs and outputs to halve the number of butterfly stages connected by a global interconnection which requires much area is presented. These algorithms can be obtained by shuffling the row and column of a decomposed FFT matrix which corresponds to one butterfly stage. Using non-recursive and recursive pipeline, the degree of serialism and parallelism in FFT computation can be adjusted. To implement high performance high radix FFT easily and reduce the amount of interconnections between stages, the method to build a high radix PE with lower radix PE 's is discussed. Finally the performances of the present architectures are evaluated and compared.

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Fe-Ti합금계에서의 충상공정조직의 열적안정성 (Thermal Stability of Lamellar Eutectic Structure in Fe-Ti Alloy)

  • 위명용;하세베 미츠히로
    • 열처리공학회지
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    • 제10권2호
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    • pp.121-127
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    • 1997
  • In order to elucidate thermal stability of Fe-$Fe_2Ti$ eutectic structure, the initial several structures have been investigated in the changes of coarsening and spheroidization during prolonged annealing under the eutectic temperature. The results are as follows: 1) The rate constant of coarsening and spheroidization was formulated as $S^{-n}-S_0^{-n}=k{\cdot}t$, where S is the total area of the interface between ${\alpha}$ and C($Fe_2Ti$) per unit volume, $S_0$ is initial value and k is the rate constant. 2) The coarsening and spheroidization mechanism was described by Ostwald ripening and controlled by diffusion of Ti-atom in ${\alpha}$-phase. 3) The spheroidization rate constant in eutectic lamellar structures was depended upon annealing temperature and showed the Arrhenius relation. The activation energy for spheroidization of lamellar structure was 365 kJ/mole.

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