• 제목/요약/키워드: Linear Cascade

검색결과 110건 처리시간 0.031초

Performance Evaluation of Cascade AOA Estimator Based on Uniform Circular Array

  • Kim, Tae-yun;Hwang, Suk-seung
    • Journal of Positioning, Navigation, and Timing
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    • 제9권2호
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    • pp.65-70
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    • 2020
  • For a wireless communication system, the angle-of-arrival (AOA) of the signal has a variety of applications. The signal AOA is estimated utilizing various antenna array structure such as Uniform Linear Array (ULA), Uniform Rectangular Array (URA), and Uniform Circular Array (UCA). In this paper, we introduce a cascade AOA estimation algorithm based on the UCA, which is consisted of CAPON and Beamspace MUSIC. CAPON is employed to estimate approximate AOA groups including multiple AOA signals and Beamspace MUSIC is employed to estimate detailed signal AOAs in the estimated AOA groups. In addition, we provide the computer simulation results for verifying and analyzing the performance of the cascade AOA estimator based on UCA.

케스케이드 실험을 위한 벽면형상 설계에 관한 연구 (A Study of Wall Shape Design for Cascade Experiment)

  • 조종현;조봉수;김재실;조수용
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.148-151
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    • 2008
  • In a double-passage cascade apparatus, only two blades are installed in order to increase the accuracy of experimental result by applying bigger blade than the size of multi-blades on the same apparatus. However, this causes difficulties to make correct periodic condition. In this study, sidewalls are designed to meet periodic condition without removing the operating fluid or adjusting tail boards. Surface Mach number on the blade surface is applied to a responsible variable, and 12 design variables which are related with sidewall profile control are selected. A gradient based optimization is adopted for wall design and CFX-11 is used for the internal flow computation. The computed result shows that it could obtain the same flow structure by modifying only the sidewalls of the double-passage cascade apparatus.

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2피치 유로 캐스케이드 실험을 위한 벽면 최적화에 관한 연구 (Optimization of sidewalls for a Double-Passage Cascade Experiment)

  • 조종현;안국영;조수용
    • 한국항공우주학회지
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    • 제36권10호
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    • pp.969-978
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    • 2008
  • 선형 캐스케이드 실험장치에서 블레이드간에 주기조건을 만족하면서 적은 개수의 블레이드를 적용하는 것은 실험의 정확도 향상뿐만 아니라 실험수행에 여러 장점을 제공한다. 따라서 본 연구에서는 유로를 캐스케이드 피치의 두 배 넓이로 설정하고 두 개의 블레이드만을 설치하였을 때 주기조건이 얻어지도록 하는 벽면의 형상설계에 관한 연구를 수행하였다. 이를 위하여 주기조건에서 얻어진 블레이드 표면에서의 마하수와 동일한 결과가 얻어지도록 목적함수를 설정하였으며, 설계변수로는 벽면의 형상과 관련이 있는 12개의 변수를 선정하였다. 벽면의 설계를 위하여 기울기 기반의 최적화법을 사용하였으며, 목적함수에 민감한 변화를 나타내는 영역의 조정과 가중치를 사용하였다. 이러한 방식으로 얻어진 결과에서 주기조건과 동일한 유동특성이 얻어질 수 있음을 확인하였다.

곡면 끝벽을 갖는 터빈 노즐 안내깃 캐스케이드내 3차원 유동장에 관한 실험적 연구 (Experimental Study on Effects of the Contoured Endwall on the Three-Dimensional Flow in a Turbine Nozzle Guide Vane Cascade)

  • 윤원남;정진택
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1975-1980
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    • 2004
  • The three-dimensional flow in a turbine nozzle guide vane passage causes large secondary loss through the passage and increased heat transfer on the blade surface. In order to reduce or control these secondary flows, a linear cascade with a contoured endwall configuration was used and changes in the three-dimensional flow field were analyzed and discussed. Measurements of secondary flow velocity and total pressure loss within the passage have been performed by means of five-hole probes. The investigation was carried out at fixed exit Reynolds number of $4.0{\times}10^5$. The objective of this study is to document the development of the three-dimensional flow in a turbine nozzle guide vane cascade with modified endwall. The results show that the development of passage vortex and cross flow in the cascade composed of one flat and one contoured endwalls are affected by the flow acceleration which occurs in contoured endwall side. The overall loss is reduced near the flat endwall rather than contoured endwall.

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160% 피치의 유로에서 단일익형에 의한 캐스케이드 실험을 위한 벽면의 설계에 관한 연구 (A Study of Design of Sidewalls for Cascade Model with Single Blade Within a 160% Pitch Passage)

  • 조종현;김영철;안국영;조수용
    • 한국항공우주학회지
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    • 제37권6호
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    • pp.527-536
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    • 2009
  • 캐스케이드 실험장치에 한 개의 익형을 설치하여 캐스케이드 실험이 가능한 장치벽면의 설계를 수행하였다. 장치의 폭은 피치의 160% 넓이이다. 이 경우에 실험장치 내에 다수개의 블레이드를 설치하는 경우에 비하여 소형의 장치라도 실험의 정확성이 향상되는 장점이 있지만, 피치방향으로 주기조건을 맞추기가 어렵다. 본 연구에서는 주기조건이 얻어지도록 벽면의 형상설계를 내부유동장의 결과를 바탕으로 기울기기반과 유전자알고리즘의 방식을 사용하여 벽면을 설계하였다. 이를 위하여 목적함수는 캐스케이드 익형의 표면에서 얻어진 마하수를 적용하였으며, 실험장치의 형상 조정이 가능한 14개의 설계변수를 적용하였다. 유전자알고리즘에 의한 최적화 설계방식이 향상된 결과를 보여주었다.

Analysis of RF-DC Conversion Efficiency of Composite Multi-Antenna Rectifiers for Wireless Power Transfer

  • Deng, Chao;Huang, Kaibin;Wu, Yik-Chung;Xia, Minghua
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제11권10호
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    • pp.5116-5131
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    • 2017
  • This paper studies the radio frequency to direct current (RF-DC) conversion efficiency of rectennas applicable to wireless power transfer systems, where multiple receive antennas are arranged in serial, parallel or cascaded form. To begin with, a 2.45 GHz dual-diode rectifier is designed and its equivalent linear model is applied to analyze its output voltage and current. Then, using Advanced Design System (ADS), it is shown that the rectifying efficiency is as large as 66.2% in case the input power is 15.4 dBm. On the other hand, to boost the DC output, three composite rectennas are designed by inter-connecting two dual-diode rectifiers in serial, parallel and cascade forms; and their output voltage and current are investigated using their respective equivalent linear models. Simulation and experimental results demonstrate that all composite rectennas have almost the same RF-DC conversion efficiency as the dual-diode rectifier, yet the output of voltage or current can be significantly increased; in particular, the cascade rectenna obtains the highest rectifying efficiency.

연소기 출구 난류 상태에서의 터빈 익열 끝벽 열(물질)전달 특성 (Endwall Heat (Mass) Transfer in a Turbine Cascade Under Combustor-Level High Free-Stream Turbulence)

  • 전상배;이상우;박병규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.759-764
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    • 2001
  • Heat (mass) transfer characteristics have been investigated on the endwall of a large-scale linear turbine cascade passage under a combustor-level high free-stream turbulence with a large length scale. Local heat (mass) transfer coefficients are measured by using the naphthalene sublimation technique. The result shows that local heat (mass) transfer on the endwall is greatly enhanced in the central region of the turbine passage, but there is no noticeable change in the local heat (mass) transfer in the region suffering severe heat load. Under the high free-stream turbulence, the local heat (mass) transfer coefficient shows more uniform distribution and its average value across the whole endwall region is increased by 26% of that at low turbulence condition. The heat (mass) transfer data on the endwall strongly supports that well-organized vortices near the endwall tends to suffer an suppression by the high free-stream turbulence.

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백라쉬를 갖는 속도제어구동 시스템의 문제점 (PROBLEMS OF A SPEED_CONTROLLED DRIVE SYSTEM WITH BACKLASH)

  • 이건용
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1989년도 추계학술대회 논문집 학회본부
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    • pp.351-354
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    • 1989
  • In a speed_controlled system with cascade control which shows an optimal performance in the linear case, limit cycles can occur due to backlash. The various effects observed can be explained with the aid of the describing function. With a first-order load torque observer these limit cycles can be avoided. Moreover the dynamic performance improves considerably and the range of application of cascade control is extended.

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선형 익렬에서의 실속 전파에 관한 수치적 해석 (Numerical Analysis of Stall Propagation in Linear Cascade)

  • 서용석;백제현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.416-421
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    • 2000
  • The performance of gas turbine engines is affected by instabilities, like as rotating stall and/or surge. Rotating Stall is a transient intermediate stage between normal flow and complete flow breakdown leading to engine surge. Rotating Stall is associated with large amplitude nonaxisymmetric flow variations rotating around the compressor annulus. This paper presents the evolutions of stall propagation in a compressor cascade by numerical analysis. The flow phenomena due to stall cells and propagation speed are examined using 2 dimensional Navier - Stokes equations.

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X-stern 배열을 가진 대형급 무인잠수정의 경로점 추적 (Waypoint Tracking of Large Diameter Unmanned Underwater Vehicles with X-stern Configuration)

  • 김도완;김문환;박호규;김태영
    • 전기학회논문지
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    • 제66권2호
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    • pp.387-393
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    • 2017
  • This paper focuses on a horizontal waypoint tracking and a speed control of large diameter unmanned underwater vehicles (LDUUVs) with X-stern configuration plane. The concerned design problem is converted into an asymptotic stabilization of the error dynamics with respect to the desired yaw angle and surge speed. It is proved that the error dynamics under the proposed control scheme based on the linear control and the feedback linearization can be considered as a cascade system; the cascade system is asymptotically stable if its nominal systems are so. This stability connection enables to separately deal with the waypoint tracking problem and the speed control one. By using the sector nonlinearity, the nominal system with nonlinearities is modeled as a polytopic linear parameter varying (LPV) system with parametric uncertainties. Then, sufficient linear matrix inequality (LMI) conditions for its asymptotic stabilizability are derived in the sense of Lyapunov stability criterion. An example is given to show the validity of the proposed methodology.