• Title/Summary/Keyword: Quasi-periodic

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The Analysis of the Airplane Flutter on Low Band Television Broadcasting Signal

  • Wonggeeratikun, A.;Noppanakeepong, S.;Leelaruji, N.;Hemmakorn, N.;Moriya, Y.
    • 제어로봇시스템학회:학술대회논문집
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    • 2003.10a
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    • pp.1648-1653
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    • 2003
  • The paper studies effect of quasi-periodic or airplane flutter phenomenon on television broadcasting signal. Airplane flutter is a very important problem. It causes the receiving antenna to receive both direct signal by the Tx (Transmitter antenna) and reflected signal scattered by the airplane with phase delay. The sum of two signals results in fading, sometime collapse and distortion of picture on TV screen. We performed measurement and modeling this phenomenon on TV signal when the airplane flew across and range Tx and Rx (Receiver antenna). The frequency 60.75MHz (Aural frequency of CH3) is used under tests. A single scatter multipath model is introduced. It is used to duplicate some of the measured data and show the dependence of power variation on the airplane fluttering. The fluctuation of the airplane flutter phenomenon was calculated to be around 2-4dB. The Yaki antenna is used for improving airplane flutter problem because it can make high gain and high directivity.

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Numerical Simulation on Laminar Flow Past a Rotary Oscillating Circular Cylinder (주기 회전하는 원형 실린더 주위 층류 유동장의 수치 시뮬레이션)

  • Park, Jong-Chun;Moon, Jin-Kuk;Chun, Ho-Hwan;Suh, Sung-Bu
    • Journal of the Society of Naval Architects of Korea
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    • v.42 no.4 s.142
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    • pp.368-378
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    • 2005
  • The effects of rotary oscillation on the unsteady laminar flow past a circular cylinder. are numerically investigated in the present study. The numerical solutions for the 20 Wavier-Stokes equation are obtained using a finite volume method Tn the framework of an overlapping grid system. The vortex formation behind a circular cylinder and the hydrodynamics of wake flows for different rotary oscillation conditions are analyzed from the results of numerical simulation. The lock-on region is defined as the region that the natural shedding frequency due to the Karmann Vortex shedding and the forcing frequency due to the forced oscillating a cylinder are nearly same, and the quasi-periodic states are observed around that region. At the intersection between lock-on and non-lock-on region the shedding frequency is bifurcated. After the bifurcation, one frequency fellows the forcing frequency($S_f$) and the other returns to the natural shedding frequency($St_0$). in the quasi-periodic states, the variation of magnitudes and relevant phase changes of $C_L$ with forcing phase are examined.

A New Pitch Detection Method Using The WRLS-VFF-VT Algorithm (WRLS-VFF-VT 알고리듬을 이용한 새로운 피치 검출 방법)

  • Lee, Kyo-Sik;Park, Kyu-Sik
    • The Transactions of the Korea Information Processing Society
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    • v.5 no.10
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    • pp.2725-2736
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    • 1998
  • In this paper. we present a new pitch determination method for speech analysis. namely VFF(Variable Forgetting Factor) based. by using the WRLS-VFF-VT(Weighted Recursive Least Square-Variable Forgetting Factor-Variable Threshold) algorithm. A proposed method uses VFF to identify the glottal closure points which correspond to the instants of the main excitation pulses for voiced speech. The modified EGG

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Compact Hybrid Branch-line Couplers and Rat-Race Couplers with Periodic Stepped Stubs (주기적인 계단형 스터브를 갖는 소형화된 하이브리드 Branch-Line 결합기와 Rat-Race 결합기)

  • Lee Chang On;Kim Won-Ki;Kim Sang-Tae;Shin Chull-Chai
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.41 no.12
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    • pp.115-124
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    • 2004
  • In this paper, we introduce the advanced compact transmission line with periodic stepped stubs. They are more effective than normal stubs in ATL. The short stepped stubs loading of transmission line work as effective shunt capacitance and that was proved by equivalent circuit based on transmission line theory and quasi-static analysis. And the compact branch-line coupler and the compact rat-race coupler via proposed compact microstrip line were designed at 1.8 ㎓. They have 677 ㎟ and 913 ㎟, respectively, and they are 62% and 45% of normal design.

The Effects of Periodic Reminding Interventions on Medication Adherence, Self-Efficacy, and Pain for Home-Based Lung Cancer Patients (주기적인 상기(Reminding) 중재가 재가 폐암환자의 진통제 복용 이행 정도, 자기효능감, 통증에 미치는 효과)

  • Shin, Jin Hee;Kim, Gwang Suk;Lee, Ju Hee;Oh, Suk Joong
    • Journal of Korean Clinical Nursing Research
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    • v.19 no.3
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    • pp.443-454
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    • 2013
  • Purpose: The purpose of this study was to evaluate the effects of periodic reminding interventions on medication adherence, self-efficacy, and pain intensity for home-based lung cancer patients. Methods: A quasi-experimental nonequivalent control group, pretest and posttest design was used. The intervention comprised of individual education by tailored image-combined medication instructions, daily reminding text message, and weekly telephone calls for four weeks. The subjects in this study consisted of 62 lung cancer patients (31 in the experimental group, and 31 in the control group). Mann-Whitney U-test was applied to analyze the data. Results: Experimental group who received periodic reminding intervention program better adhered to prescribed medication compared to the control group (z=-6.14, p<.001). Experimental group demonstrated higher level of self-efficacy compared to the control group (z=-6.74, p<.001). Experimental group experienced less intense average pain compared to the control group (z=-6.29, p<.001). Conclusion: The findings suggest that periodic reminding interventions can be applied as an effective nursing intervention to promote medication adherence and self-efficacy to improve and pain management for home-based lung cancer patients.

RADIAL AND AZIMUTHAL OSCILLATIONS OF HALO CORONAL MASS EJECTIONS

  • Lee, Harim;Moon, Y.J.;Nakariakov, V.M.
    • The Bulletin of The Korean Astronomical Society
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    • v.40 no.1
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    • pp.66.1-66.1
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    • 2015
  • We present the first observational detection of radial and azimuthal oscillations in full halo coronal mass ejections (HCMEs). We analyze nine HCMEs well-observed by LASCO from Feb 2011 to Jun 2011. Using the LASCO C3 running difference images, we estimated the instantaneous apparent speeds of the HCMEs in different radial directions from the solar disk center. We find that the development of all these HCMEs is accompanied with quasi-periodic variations of the instantaneous radial velocity with the periods ranging from 24 to 48 mins. The amplitudes of the instant speed variations reach about a half of the projected speeds. The amplitudes are found to anti-correlate with the periods and correlate with the HCME speed, indicating the nonlinear nature of the process. The oscillations have a clear azimuthal structure in the heliocentric polar coordinate system. The oscillations in seven events are found to be associated with distinct azimuthal wave modes with the azimuthal wave number m=1 for six events and m=2 for one event. The polarization of the oscillations in these seven HCMEs is broadly consistent with those of their position angles with the mean difference of $42.5^{\circ}$. The oscillations may be connected with natural oscillations of the plasmoids around a dynamical equilibrium, or self-oscillatory processes, e.g. the periodic shedding of Alfvenic vortices. Our results indicate the need for advanced theory of oscillatory processes in CMEs.

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Fluttering Characteristics of Free-falling Plates (자유낙하하는 판의 fluttering 특성 연구)

  • Hong, Seulki;Chae, Seokbong;Kim, Jooha
    • Journal of the Korean Society of Visualization
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    • v.15 no.2
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    • pp.33-40
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    • 2017
  • Abstract In the present study, the characteristics of kinematics and dynamics in the fluttering motion of free-falling plates are investigated at Reynolds number of $10^5$. We record quasi-two-dimensional trajectories of free-falling plates with and without superhydrophobic coating using high-speed camera, and compute the drag and lift forces by trajectory analysis. Translational and angular velocities are modeled as harmonic functions with specific phase differences. In particular, periodic mass elevations near turning points are explained using the suggested models. At each turning point, a sudden drop in lift and a rapid increase in drag occur simultaneously due to fast increase in angle of attack. However, the lift is increased over the buoyancy-corrected weight of plate during gliding flight, resulting in periodic mass elevations near turning points. Superhydrophobicity is shown to increase lift but to reduce drag on a fluttering plate, resulting in the decrease of mean descent speed.

Comparative Behavior Analysis in Love Model with Same and Different Time Delay (동일 시간 지연과 서로 다른 시간 지연을 갖는 사랑모델에서의 비교 거동 해석)

  • Huang, Linyun;Ba, Young-Chul
    • Journal of the Korean Institute of Intelligent Systems
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    • v.25 no.3
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    • pp.210-216
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    • 2015
  • It is well known that the structure of brain and consciousness of human have a phenomena of complex system. The human emotion have a many kind. The love is one of human emotion, which have been studied in sociology and psychology as a matter of great interested thing. In this paper, we consider a same and different time delay in love equation of Romeo and Juliet. We represent a behavior of love as a time series and phase portrait, and analyze the difference of behaviors between a same and different time delay.

Diagnosis of HSC Convective Flow Using a Digital Holographic Interferometry and PIV System (디지털 홀로그래픽 간섭계와 PIV를 이용한 Hele-Shaw Cell 내부 열유동 해석)

  • Kim, Seok;Lee, Sang-Joon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.4
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    • pp.493-499
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    • 2004
  • Variations of temperature and velocity fields in a Hele-Shaw convection cell (HSC) were investigated using a holographic interferometry and 2-D PIV system with varying Rayleigh number. To measure quasi-steady variation of temperature field, two different measurement methods of holographic interferometry, double-exposure method and real-time method, were employed. In the double-exposure method, unwanted waves were eliminated effectively using a digital image processing technique. The reconstructed images are clear, but transient flow cannot be reconstructed clearly. On the other hand, transient convective flow can be reconstructed well using the real-time method. However, the fringe patterns reconstructed by the real-time method contain more noises, compared with the double-exposure method. Experimental results show a steady flow pattern at low Rayleigh numbers and a time-dependent periodic flow structure at high Rayleigh numbers. The periodic flow pattern at high Rayleigh numbers obtained by the real-time holographic interferometer method is in a good agreement with the PIV results.

Direct Numerical Simulation of the Flow Past an Oscillating Circular Cylinder (진동하는 원주주위 유동의 직접수치해석)

  • Kang S. J.;Tanahashi M.;Miyauchi T.;Lee Y. H.
    • Journal of computational fluids engineering
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    • v.6 no.4
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    • pp.26-34
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    • 2001
  • The flow past a circular cylinder forced to vibrate transversely is numerically simulated by solving the two-dimensional Navier-Stokes equations modified by the vibration velocity of a circular cylinder at a Reynolds number of 164. The higher-order finite difference scheme is employed for the spatial discretization along with the second order Adams-Bashforth and the first order backward-Euler time integration. The calculated cylinder vibration frequency is between 0.60 and 1.30 times of the natural vortex-shedding frequency. The calculated oscillation amplitude extends to 25% of the cylinder diameter and in the case of the lock-in region it is 60%. It is made clear that the cylinder oscillation has influence on the wake pattern, the time histories of the drag and lift forces, power spectral density and phase diagrams, etc. It is found that these results include both the periodic (lock-in) and the quasi-periodic (non-lock-in) state. The vortex shedding frequency equals the driving frequency in the lock-in region but is independent in the non-lock-in region. The mean drag and the maximum lift coefficient increase with the increase of the forcing amplitude in the lock-in state. The lock-in boundaries are also established from the present direct numerical simulation.

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