• Title/Summary/Keyword: 유동공진

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Excremental Study on Wave Drag in Supersonic Wavy Walls (초음속 파동 벽면에서의 조파저항에 관한 실험적 연구)

  • Kwon, Min-Chan;Semenov, Vasily V.
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.758-759
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    • 2010
  • In this study, it was experimentally confirmed that the phenomenon of resonance effect of wave drag in two wavy walls. The channel had saw-tooth type of relief surfaces when supersonic gas flows into this channel. Experiment was carried out on the differential apparatus by conducting the comparative test of two nozzles (round sonic nozzle and two-dimensional nozzle with wavy walls). The two-dimensional nozzle was joined alternately with flat walls which had saw-tooth type of symmetrical and asymmetric reliefs. Two-dimensional nozzle was designed for the M=3 and profiled parabolic contour.

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Zero-voltage-switching three level auxiliary resonant commutated pole inverter (영전압 스위칭 3-레벨 보조 공진 폴 인버터)

  • 유동욱;원충연;조정구;백주원
    • The Transactions of the Korean Institute of Electrical Engineers
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    • v.45 no.4
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    • pp.535-542
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    • 1996
  • A zero voltage switching (ZVS) three level auxiliary resonant commutated pole inverter (ARCPI) is presented for high power GTO inverters. The concept of ARCP for two level inverter is extended to the three inverter. The proposed auxiliary commutation circuit consists of one resonant inductor and two bi-directional switches, which provides ZVS condition to the main devices without increasing device voltage or current stresses. The auxiliary device operates with zero current switching (ZCS) which enables use of the low cost thyristors. The proposed ARCPI can handle higher voltage and higher power (1-10MVA) comparing to the two level one. Operation and analysis of the ARCPI are illustrated and the features are compared o those of the snubber circuit incorporated three level inverter. Experimental results with 10kW, 4kHz prototype are presented to verify the principle of operation. (author). refs., figs., tab.

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The Application of the Induction Heating Technology for the food dryness (식품건조를 위한 유도가열 기술 응용 연구)

  • Ryu M.H.;Baek J.W.;Kim J.H.;Yoo D.W.;Rim G.H.
    • Proceedings of the KIEE Conference
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    • summer
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    • pp.1148-1150
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    • 2004
  • 본 논문에서는 $400^{\circ}C$ 이상의 과열 증기발생을 위하여 6kW급 유도가열장치를 개발하여 식품건조 시스템에 적용한 예를 보인다. 유도가열장치는 과열 증기의 온도를 제어하기 위하여 인버터 입력 전압을 $100\sim200V$로 가변제어가 가능하게 하였고, 인버터 입력 전압은 벅컨버터를 사용하여 기준 전압을 과열증기의 온도에 대한 전압 값을 사용하여 제어하였으며, LC 공진에 의해 발생한 전류로 증기 가열 챔버를 유도 가열하여 과열 증기를 발생하게 하였다. 발생한 과열 증기는 식품 건조를 위하여 건조로에 투입되어 고온 건조에서 식품의 건조시간을 단축시킬 수 있었으며, 식품의 손상을 줄일 수 있었다. 이의 검증을 위하여 유도 가열 장치를 설계/제작하여 실험하였으며, 식품 건조 테스트를 행하였다.

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Control Strategy of Resonant DC Link Inverter for UPS (UPS용 병렬공진형 직류링크인버터를 위한 제어방식에 관한 연구)

  • Beak, J.W.;Yoo, D.W.;Min, B.G.;Ryu, S.P.
    • Proceedings of the KIEE Conference
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    • 1994.11a
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    • pp.159-161
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    • 1994
  • A new control technique which generates high-quality sinusoidal output voltage from a single-phase resonant do link inverter suitable for the UPS systems is presented. The inverter output voltage control system has the PID controller with a minor loop of the filter inductor current and tile feedforward controller. The proposed control scheme also solves resonant voltage overshoot without any additional switch or passive component, resulting in pulses with uniform amplitude and high efficiency. Experimental results in the case of linear and nonlinear loads are presented to confirm the usefulness of the Proposed control algorithms.

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A Novel ZVS 3-Level Resonant Pole Inverter (새로운 ZVS 3-레벨 공진폴 인버터)

  • Baek, Ju-W.;Cho, Jung-G.;Yoo, Dong-W.;Song, Doo-I.;Won, Cung-Y.
    • Proceedings of the KIEE Conference
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    • 1995.07a
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    • pp.360-364
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    • 1995
  • A zero voltage switching (ZVS) three level resonant pole inverter is presented for high power GTO inverters. The concept of auxiliary resonant commutated pole(ARCP) for two level inverter is extended to the three level inverter. The proposed auxiliary commutation circuit consists of one resonant inductor and two bi-directional switches, which provides ZVS condition to the main devices without increasing device voltage or current stresses. The auxiliary device operates with zero current switching(ZCS) which enables use of the low cost thyristors. The proposed circuit can handle higher voltage and higher power(1-10MVA) comparing to the two level one. Operation and analysis of the proposed circuit are illustrated. Experimental results with 10 KW, 4 kHz prototype are presented to verify the principle of operation.

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A Study on High Frequency Resonant Type X-ray Generator (고주파 공진형 방식 X-선 발생장치에 관한 연구)

  • Yoo, Dong-Wook;Ha, Sung-Woon;Baek, Joo-Won;Kim, Jong-Soo;Kim, Hack-Seong;Won, Chung-Yuen
    • Proceedings of the KIEE Conference
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    • 1995.07a
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    • pp.209-211
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    • 1995
  • This paper is concerned with High Frequency, High Voltage Generator for X-ray using zero-voltage soft-switching PWM DC-DC high-power converter by Resonant method, which makes the most of the parastic LC parameters of high-voltage transformer link, for diagnostic X-ray power generator. The converter circuit basically utilizes phase-shift pulse width modulated series Resonant full-bridge PWM DC-DC high-power converter operating at a constant frequency;25kHz. The converter output regulation is digitally controlled using DSP (Digital Signal Processor) for obtaining a fast rising time and adjust output voltage within a wide load range.

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Vortex sheddings and Pressure Oscillations in Hybrid Rocket Combustion (하이브리드로켓 연소실의 와류발생과 연소압력 진동)

  • Park, Kyungsoo;Shin, Kyung-Hoon;Lee, Changjin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.1
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    • pp.40-47
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    • 2013
  • The similarity in internal flow of solid and hybrid rocket suggests that hybrid rocket combustion can be susceptible to instability due to vortex sheddings and their interaction. This study focuses on the evolution of interaction of vortex generated in pre-chamber with other types of vortex in the combustor and the change of combustion characteristics. Baseline and other results tested with disks show that there are five different frequency bands appeared in spectral domain. These include a frequency with thermal lag of solid fuel, vortex shedding due to obstacles such as forward, backward facing step and wall vortices near surface. The comparison of frequency behavior in the cases with disk 1 and 3 reveals that vortex shedding generated in pre-chamber can interact with other types of vortex shedding at a certain condition. The frequency of Helmholtz mode is one of candidates resulting to a resonance when it was excited by other types of oscillation even if this mode was not discernable in baseline test. This selective mechanism of resonance may explain the reason why non-linear combustion instability occurs in hybrid rocket combustion.

Analysis of Sloshing Frequency Response in Rectangular Fuel-Storage Tank (사각형 연료탱크 내 슬로싱 주파수 응답 해석)

  • 조진래;이홍우;하세윤;박태학;이우용
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.16 no.1
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    • pp.95-104
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    • 2003
  • This paper deals with the analytic and FEM analyses of sloshing frequency response of incompressible, invicid and irrotational flow in two dimensional rectangular tank. We use Laplace equation based on potential theory as governing equation. For small amplitude sloshing motion, the linearized free surface condition was applied and the analytic solution as obtained by the separation of variables. To simulate the effect of the energy dissipation due to viscous damping, artificial viscous coefficient is introduced and the divergence of response at resonance frequencies may be avoided by this coefficient. This problem was solved by FEM using 9-node elements in order to predict the maximum amplitude of sloshing response. Numerical results of free surface height, fluid pressure and fluid force show good agreement with those by analytic solution. After verifying the test FEM program, we analyze the frequency response characteristics of sloshing to the fluid height.

Experimental Study on Flow Structure of Wake Behind a Rotationally Oscillating Circular Cylinder (주기적으로 회전진동하는 원주 후류의 유동구조에 관한 실험적 연구)

  • Lee Jung-Yeop;Lee Sang-Joon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.30 no.4 s.247
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    • pp.298-305
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    • 2006
  • The flow around a circular cylinder which oscillates rotationally with a relatively high forcing frequency has been investigated experimentally using flow visualization and hot-wire measurements. Dominant parameters are Reynolds number (Re), oscillation amplitude $({\theta}_A)$, and frequency ratio $F_R=f_f/f_n$, where $f_f$ is the forcing frequency and $f_n$ is the natural frequency of vortex shedding. Experiments were carried out under the conditions of $Re=4.14{\times}10^3,\;{\theta}_A={\pi}/6$, and $0{\leq}F_R{\leq}2$. The effect of frequency ratio $F_R$ on the flow structure of wake was evaluated by measuring wake velocity profile and spectral analysis of hot-wire signal. Depending on the frequency ratio $F_R$, the cylinder wake has 5 different flow regimes. The vortex formation length and vortex shedding frequency are changed significantly before and after the lock-on regime. The drag coefficient was reduced under the condition of $F_R<1.0$ and the maximum drag reduction is about 33% at $F_R=0.8$. However, the drag is increased as $F_R$ increases beyond $F_R=1.0$. This active flow control method can be effective in aerodynamic applications, if the forcing parameters are selected optimally.

Acoustic Levitation and Rotation Produced by Ultrasonic Flexural Vibration (초음파 굽힘 진동에 의한 음향 부상 및 회전)

  • Loh, Byoung-Gook
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.14 no.5
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    • pp.432-438
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    • 2004
  • Acoustic levitation induced by ultrasonic flexural vibration at 28.4 KHz with a vibration amplitude of 10 micrometers is presented. Levitation of multiple objects along the length of the beam in a gap of 8.3 mm which is the half of acoustic wavelength is experimentally demonstrated. Analytical analysis predicts that levitated objects for the gap of half-the wavelength converges to the center of the gap, which is experimentally verified. It is observed that levitated objects with well-balanced mass distribution are set into rotation due to acoustic streaming. For cylinder-shaped Styrofoam with a diameter of 1.8 mm and a length of 3 mm, measured rotational velocity is 2400 revolution per minute. Applications of standing wave field levitation (SWFL) include manipulation of biological cells and blood constituents in biotechnology, and fine powder in material engineering.