• Title/Summary/Keyword: 파워 스펙트럼 밀도

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On the Estimation Techniques of Hurst exponent (허스트 지수 산정 방법에 대한 고찰)

  • Kim, Byung-Sik;Kim, Hung-Soo;Seoh, Byung-Ha
    • Journal of Korea Water Resources Association
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    • v.37 no.12
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    • pp.993-1007
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    • 2004
  • There are many different techniques for the estimation of the Hurst exponent. However, the techniques can produce different characteristics for the persistence of a time series each other. This study uses several techniques such as adjusted range, resealed range(RR) analysis, modified restated range(MRR) analysis, 1/f power spectral density analysis, Maximum Likelihood Estimation(MLE), detrended fluctuations analysis(DFA), and aggregated variance time(AVT)method for the Hurst exponent estimation. The generated time series from chaos and stochastic systems are analyzed for the comparative study of the techniques. Then this study discusses the advantages and disadvantages of the techniques and also the limitations of them.

Evaluation of the Acceleration-factor and Analysis of the Vibration Fatigue for the Connection-pipe to the Compressor under the Random Vibration (랜덤 진동 조건에서의 압축기 연결 파이프에 대한 가속 수명 팩터 선정 및 진동 피로 해석)

  • Han, Hyung-Suk;Jung, Woo-Seoung;Yoon, Kyung-Jong;Mo, Jin-Yong
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.18 no.3
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    • pp.323-334
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    • 2008
  • According to the delivery condition, the breakage of a product occurs when it is delivered to the customers. Therefore product's makers evaluate the durability under the delivery process by accelerated life testing. In order to conduct this accelerated life testing accurately, it is very important to identify the acceleration-factor exactly between on-road and accelerated life test condition. In this paper, the acceleration-factor is identified by applying linear damage summation law, rain-flow cycle counting and Dirlik theory under the conditions of the random vibration. And approximated FEM model of the connecting-pipe to the compressor is developed for fatigue analysis. This model is finally verified by comparing the experiment results to the numerical analysis results.

Evaluation of Vehicle Body Stiffness by Measuring Local Vibration (위치별 진동 측정을 통한 차체강성평가)

  • Lee, Kyung Tae;Jun, Yong Du;Choi, Doo Seuk
    • Transactions of the Korean Society of Automotive Engineers
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    • v.21 no.6
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    • pp.195-200
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    • 2013
  • Road loads data are indispensable in the evaluation of BSR (Buzz, Squeak, and Rattle) of automotive parts/modules. However, there are uncertainties on the best measurement locations for representative body motion and for seat systems. In the present study, we measure road loads at four different locations of a body. A-pillars on the driver and passenger sides and left and right frame fronts of the front passenger seat mountings are selected to study the acceleration behavior at different locations. The measurements are conducted with passenger cars driving local roads at 50km/hr. The measured time-acceleration data are then transformed into PSD (power spectral density) data to compare the characteristics of local accelerations. By defining the deviated acceleration components from rigid body motion, the stiffness of vehicle body could be simply expressed in a quantitative basis. Measured data from two different vehicles are presented to demonstrate their relative vehicle body stiffness.

A Study on the Development of Vehicle Dynamic Model for Dynamic Characteristics Analysis of Chassis Parts (샤시부품 동특성 해석을 위한 전차량 해석모델 개발에 관한 연구)

  • Bae, Chul-Yong;Kwon, Seong-Jin;Kim, Chan-Jung;Lee, Bong-Hyun;Na, Byung-Chul
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.17 no.10
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    • pp.958-966
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    • 2007
  • This study presents full vehicle dynamics model for the dynamic characteristic analysis of chassis parts which are suspension and brake system. This vehicle dynamics model is appled to kinematics and quasi-static analysis for each chassis part. In order to develop the vehicle dynamics model, the parameters of each chassis element part which are bush, spring and damper are measured by experiment. Also the wheel forces and moments of 6 DOF are measured at each wheel center. These data are applied to input parameter for vehicle dynamics model. And the verification of the developed model is achieved to comparison with the experimental force data of spring, trailing arm and assist arm by using the load response by strain gauge. These experimental force data are acquired by road test at event surfaces of P/G which are belgian and chuck holes roads.

Development of a 9as-liquid two-phase flowmeter using double orifice plates (2중판 오리피스를 이용한 기액 2상유량계의 개발)

  • 이상천;이상무;남상철
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.10 no.5
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    • pp.619-629
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    • 1998
  • An experimental work was conducted to investigate a feasibility of simultaneous measurement of gas-liquid two-phase flowrates with double orifice plates using air and water. The tests were carried out under the atmospheric pressure and at the ambient temperature using two different tube sizes. Qualities of an air-water flow in the present study have values less than 0.1 and thus the mixed flow showed bubbly, plug, slug flow regimes. The probability density function (PDF) and the power spectral density function (PSDF) of the instantaneous pressure drop traces for the flow regimes were obtained. It is found that some distinctive features exist in the distribution of these functions, depending upon the two-phase flow pattern. The time-averaged value of the instantaneous pressure drop increases with increasing gas and liquid flowrates, showing a single-valued function for the total mass flowrate and the quality. It is also found that the two-phase discharge coefficient exhibits a consistent trend for variation of dimensionless parameters such as the superficial velocity ratio and the gas Reynolds number. The results indicate that simultaneous measurement of two-phase flowrate may be possible based upon a statistical analysis of the instantaneous pressure drop curves monitored using double orifice plates.

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Design of Tower Damper Gain Scheduling Algorithm for Wind Turbine Tower Load Reduction (풍력터빈 타워 하중 저감을 위한 타워 댐퍼 게인 스케줄링 알고리즘 설계)

  • Kim, Cheol-Jim;Kim, Kwan-Su;Paek, In-Su
    • Journal of the Korean Solar Energy Society
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    • v.38 no.2
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    • pp.1-13
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    • 2018
  • This paper deals with the NREL (National Renewable Energy Laboratory) 5-MW reference wind turbine. The controller which include MPPT (Maximum power point tracking) control algorithm and tower load reduction control algorithm was designed by MATLAB Simulink. This paper propose a tower damper algorithm to improve the existing tower damper algorithm. To improve the existing tower damper algorithm, proposed tower damper algorithm were applied the thrust sensitivity scheduling and PI control method. The thrust sensitivity scheduling was calculated by thrust force formula which include thrust coefficient table. Power and Tower root moment DEL (Damage Equivalent Load) was set as a performance index to verify the load reduction algorithm. The simulation were performed 600 seconds under the wind conditions of the NTM (Normal Turbulence Model), TI (Turbulence Intensity)16% and 12~25m/s average wind speed. The effect of the proposed tower damper algorithm is confirmed through PSD (Power Spectral Density). The proposed tower damper algorithm reduces the fore-aft moment DEL of the tower up to 6% than the existing tower damper algorithm.

A Study on the Flight Vibration Environmental Specification of Unmanned Flying Vehicle using Random Vibration Test and Analysis Methods (랜덤 진동 시험 및 해석 기법을 이용한 무인 비행체의 비행 진동 환경 규격 연구)

  • Jangseob, Choi;Dongho, Oh
    • Journal of the Korea Institute of Military Science and Technology
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    • v.25 no.6
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    • pp.596-605
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    • 2022
  • In this study, analysis of dynamic characteristics and flight vibration was performed to unmanned aerial vehicles. The analysis model was supplemented by performing a dynamic characteristic test and a random vibration test using manufactured dummy aerial vehicle. For the dynamic characteristic test, a bungee cable was used to implement the free end boundary condition. Prior to the flight vibration test using a multiple electric shaker, a random vibration test was performed to predict the excitation force during the actual flight vibration test. It was judged that the actual test could be predicted more accurately by supplementing the analysis model from the test results. In addition, it was possible to determine the feasibility of the test by predicting the excitation force of the flight vibration test.

A Study On Flight Vibration Environmental Test of Unmanned Aerial Vehicle using Dual Electric Vibration Exciters (이중 전동식 진동 시험기를 이용한 무인 비행체의 비행진동 환경시험 연구)

  • Jangseob Choi;Dongho Oh
    • Journal of the Korea Institute of Military Science and Technology
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    • v.26 no.3
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    • pp.252-261
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    • 2023
  • Analysis of dynamic characteristics and flight vibration test for unmanned aerial vehicles was studied by using dummy test body. The FEM model for dummy test body was supplemented by results of modal and random vibration test. The free end boundary condition to simulate flight environments was made by test setup using bungee cable. Prior to the flight vibration test using a dual electric vibration exciters, the test procedure to calculate quantitative vibration level was studied by using military specification. The actual test was successfully done by using the analysis and pretest results. From the analysis results, it was possible to determine the feasibility of the test by predicting the excitation force of the flight vibration test and to get the response of any point which could not be measured by the test. The results of this study will much contribute to the Test and Evaluation of unmanned aerial vehicles.

컷오프 진단법을 이용한 고속 측정법

  • Na, Byeong-Geun;Yu, Gwang-Ho;Lee, Yun-Seong;Jang, Hong-Yeong
    • Proceedings of the Korean Vacuum Society Conference
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    • 2011.02a
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    • pp.201-201
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    • 2011
  • 컷오프 진단법은 프로브 형태로 제작된 마이크로 웨이브 진단법으로, 간단한 수식을 통해 전자밀도, 전자온도 등의 측정이 가능하며, 장치나 분석방법이 매우 간단한 장점을 지닌다. 또한, 측정에 약 1 mW 정도의 적은 파워를 사용하여 플라즈마 상태를 거의 변화시키지 않으며, 공정 플라즈마에서도 사용이 가능하다. 그러나 컷오프 진단법을 사용한 측정은 다른 종류의 프로브와 마찬가지로, 약 1초 정도의 긴 시간이 필요로 하는 단점이 있다. 따라서 기존의 컷오프 진단법은 펄스 플라즈마나 토카막과 같이 빠르게 변하는 플라즈마를 측정하기에는 무리가 있다. 본 발표에서는 컷오프 진단법을 새로운 방법으로 구현하여 더욱 빠르게 측정할 수 있는 방법을 소개하고자 한다. 컷오프 프로브는 방사 안테나, 측정 안테나와 네트워크 분석기로 구성되어 있다. 네트워크 분석기는 두 안테나 사이의 플라즈마 투과 스펙트럼을 만드는데 쓰이며, 주파수 스캔 방법을 사용하여 스펙트럼을 만든다. 컷오프 진단법의 측정시간은 주파수 스캔에 걸리는 시간에 의해 결정된다. 본 발표에서는 측정을 빠르게 하고자 전혀 새로운 방법을 도입하였다. 펄스 형태의 단일신호를 플라즈마 투과 특성을 살피는데 이용하면 측정을 매우 빠르게 할 수 있다. 그래서 펄스제조기와 오실로스코프를 이용하여 스펙트럼을 얻는데 사용하였다. 이론적으로는 이 방법을 통해 측정시간을 수 nano second 수준으로 줄일 수 있다. 실험적으로는 micro second 정도의 시간으로 측정을 할 수가 있었으며, 동일한 스펙트럼 및 측정결과를 얻을 수 있었다. 또한 이 방법을 펄스플라즈마에 적용할 경우 수십 nano second 수준의 시간분해능으로 측정을 할 수가 있었다. 이 방법을 응용하면 토카막 언저리와 같이 매우 빠르게 변하며 반복되지 않는 플라즈마의 측정도 가능할 것으로 예상된다.

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A study on the Structure of Turbulent Diffusion Flame Behind the Hollowed Flame Holder (중앙분공형 보염기 후류에 안정된 난류확산화염의 구조에 관한 연구(I))

  • Kang, I.G.;Lee, W.S.;Kim, T.H.;Lee, D.H.
    • Journal of Power System Engineering
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    • v.2 no.2
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    • pp.13-19
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    • 1998
  • The purpose of study is to investigate the flame stability and Structure of turbulent diffusion flame behind the hollowed flame holder, which is located on the waste gas coming out from the test furnace. Fluctuating temperature and ion current measurement and their statistical treatment were used for the purpose. Three types of flame were stabilized and each of which were changed by adequate equivalence ration. And we found that have no periodicity near reacting zone.

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