• Title/Summary/Keyword: 진폭계수

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Unsteady Aerodynamic Characteristics of an Non-Synchronous Heaving and Pitching Airfoil Part 2 : Pitching Amplitude (비동기 히브 및 피치 운동에 따른 에어포일 비정상 공력 특성 Part 2 : 피치 진동운동 진폭)

  • Seunghwan Ji;Cheoulheui Han
    • Journal of Aerospace System Engineering
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    • v.17 no.6
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    • pp.63-71
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    • 2023
  • In the present study, the effect of pitch amplitude on the unsteady aerodynamics of a NACA 0012 airfoil is numerically investigated. When the frequency ratio is equal to 1.0, airfoil pitching with 20 and 30 degrees of pitch amplitude shows almost small lift generation, but the lift is significantly increased in case of 10-degree pitch amplitude. When the frequency is 0.5, the lift coefficients have large values, and the lift increases with a decrease in pitch amplitude. When the frequency ratio is 1.0, the airfoil generates large thrust. The thrust decreases as the pitch amplitude decreases. When the frequency ratio is 0.5, drag is generated for the 30-degree pitch amplitude, but the thrust is generated for 10-degree pitch amplitude. In future, the effect of heave amplitude on the unsteady aerodynamics of the airfoil will be studied.

Privacy-Preserving Clustering on Time-Series Data Using Fourier Magnitudes (시계열 데이타 클러스터링에서 푸리에 진폭 기반의 프라이버시 보호)

  • Kim, Hea-Suk;Moon, Yang-Sae
    • Journal of KIISE:Databases
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    • v.35 no.6
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    • pp.481-494
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    • 2008
  • In this paper we propose Fourier magnitudes based privacy preserving clustering on time-series data. The previous privacy-preserving method, called DFT coefficient method, has a critical problem in privacy-preservation itself since the original time-series data may be reconstructed from privacy-preserved data. In contrast, the proposed DFT magnitude method has an excellent characteristic that reconstructing the original data is almost impossible since it uses only DFT magnitudes except DFT phases. In this paper, we first explain why the reconstruction is easy in the DFT coefficient method, and why it is difficult in the DFT magnitude method. We then propose a notion of distance-order preservation which can be used both in estimating clustering accuracy and in selecting DFT magnitudes. Degree of distance-order preservation means how many time-series preserve their relative distance orders before and after privacy-preserving. Using this degree of distance-order preservation we present greedy strategies for selecting magnitudes in the DFT magnitude method. That is, those greedy strategies select DFT magnitudes to maximize the degree of distance-order preservation, and eventually we can achieve the relatively high clustering accuracy in the DFT magnitude method. Finally, we empirically show that the degree of distance-order preservation is an excellent measure that well reflects the clustering accuracy. In addition, experimental results show that our greedy strategies of the DFT magnitude method are comparable with the DFT coefficient method in the clustering accuracy. These results indicate that, compared with the DFT coefficient method, our DFT magnitude method provides the excellent degree of privacy-preservation as well as the comparable clustering accuracy.

A Numerical Study of Aerodynamic Characteristics in Oscillating Airfoils along Frequencies and Amplitude (진동하는 익형의 진동수와 받음각 진폭에 따른 공력특성)

  • Lee, Gang-Mun;Park, Jae-Yeong;Lee, Seong-Gi
    • Proceeding of EDISON Challenge
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    • 2015.03a
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    • pp.569-574
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    • 2015
  • 지난 수십 년간 유체역학적인 관점에서 곤충이나 새의 움직임을 모방하기 위해 진동하는 익형(pitching airfoil)과 동적 실속에 관한 많은 연구가 진행되어 왔다. 그러나 유동박리가 일어나지 않는 범위 내에서 진동하는 익형의 특성에 대한 연구는 보기 드물다. 또한 기존의 유동박리가 일어나지 않는 영역에서 익형의 진동 현상에 대해 수행된 연구는 수중과 같이 낮은 레이놀즈수에서 수렴되었기 때문에, 공기 중과 같이 높은 레이놀즈수에서 유동현상과 다른 특성을 보여주고 있을 수 있다. 따라서 본 연구는 높은 레이놀즈수에서의 다양한 환산 진동수, 받음각진폭, 익형에 따른 공력특성을 분석하였다. 그 결과, 익형의 진동으로 인한 양력계수의 차이는 작음을 알 수 있었다. 그러나 높은 환산 진동수에서 익형의 항력계수가 감소하는 경향이 나타나며, 이로 인해 높은 환산 진동수에서 수치적으로 추력이 발생할 수 있음을 확인하였다.

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A Neural Networks Approach to Voiced-Unvoice-Silence Classification Incorporating Amplitude Distribution (음성 진폭분포로 신경망을 구동한 유-무-묵음 분류)

  • 이인섭;최정아;배명진;안수길
    • The Journal of the Acoustical Society of Korea
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    • v.9 no.6
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    • pp.15-21
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    • 1990
  • 유-무-묵음 분류 과정은 음성분석시에 아주 중요한 문제중의 하나이다. 음성에너지, ZCR, 자기 상관계수, LPC 계수, 예측에러 에너지등을 퍼래미터로 사용하여 지금까지 많은 분류기법이 제안되어져 왔다. 이런기법들은 기본적으로 퍼래미터를 추출해야 하고, 이 때문에 많은 계산량이 요구되고, 이들 퍼 래미터는 음성 본래의 정보들의 대부분을 상실하게 된다. 이 때문에 각 프레임의 진폭분포를 사용하는 새로운 앨고리즘을 제안하였다. 첫째로 V-U-S 영역은 개별 진폭분포형태를 가지기 때문에 주어진 프레 임에서 진폭분포를 구한다. 그런 다음에는 신경망을 통해 분류를 하게 된다. 신경망은 문덕값을 별도로 선정할 필요없고, 배경잡음에 강력하며, 또한 실시간 처리에 적합하다.

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Rheological Characteristics of Polyaniline Suspension as an Electrorheological Fluid (전기유변유체로서의 폴리아닐린 현탁액의 유변학적 특성)

  • 권무현
    • The Korean Journal of Rheology
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    • v.7 no.3
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    • pp.203-210
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    • 1995
  • 전기장 하에서 폴리아닐린/미네랄 오일 현탁액의 유변학적 특성에 관한 실험적인 연 구를 큐엣 셀 형태의 레오미터를 사용하여수행하였다. 폴리아닐린 현탁액은 전기장을 가해 줄 때 점도가 크게 상승하는 현상을 보였고 부피분율과 전기장의 3/2승에 비례하는 동적 항 복응력을 나타내었다. 작은 변형 진폭의 동적 상태 실험을 통하여 저장계수와 손실계수를 변형진폭, 변형의 구동 주파수 및 전기장의 함수로 나타내었다. 저장계수는 전기장을 증가시 킬 때 증가하나 손실계수(5wt%)는 약한 전기장 의존성을 보였다. 낮은 응력을 가해줄때의 크립과 회복곡선은 초기의 순간적인 변형 증가와 지연되는 변형 그리고 회복 불가능한 영구 적 변형으로 구성되어진다. 탄성 한계 항복응력은 전기장의 세기가 증가함에 따라 증가하였 다. 매우 작은 변형에서는 응력과 변형사이의 선형적 관계를 보여 고체와 유사한 거동을 나 타내었다.

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A Study on Determination of Gradient Coefficients in the New Evaluation of Collision Risk (신 충돌위험도평가의 기울기계수 결정에 관한 연구)

  • Jeong, Tae-Gweon
    • Journal of Navigation and Port Research
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    • v.27 no.4
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    • pp.351-357
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    • 2003
  • Evaluating the risk of collision quantitatively plays a key role in developing the expert system of navigation and collision avoidance. This study analysed theoretically and thoroughly how to determine the gradient coefficients as described in the new evaluation of collision risk using sech function, and suggested the appropriate values as applicable.

AVO analysis using crossplot and amplitude polynomial methods for characterisation of hydrocarbon reservoirs (탄화수소 부존구조 평가를 위한 교차출력과 진폭다항식을 이용한 AVO 분석)

  • Kim, Ji-Soo;Kim, Won-Ki;Ha, Hee-Sang;Kim, Sung-Soo
    • Geophysics and Geophysical Exploration
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    • v.14 no.1
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    • pp.25-41
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    • 2011
  • AVO analysis was conducted on hydrocarbon-bearing structures by applying the crossplot and offset-coordinate amplitude polynomial techniques. To evaluate the applicability of the AVO analysis, it was conducted on synthetic data that were generated with an anticline model, and field data from the hydrocarbon-bearing Colony Sand bed in Canada. Analysis of synthetic data from the anticline model demonstrates that the crossplot method yields zero-offset reflection amplitude and amplitude variation with negative values for the upper interface of the hydrocarbon-bearing layer. The crossplot values are clustered in the third quadrant. The results of AVO analysis based on the coefficients of the amplitude polynomial are similar to those from the crossplots. These well correlated results of AVO analysis on field and synthetic data suggest that both methods successfully investigate the characteristics of the reflections from the upper interface of a hydrocarbon-bearing layer. Analysis based on the incident-angle equation facilitates the application of various interpretation methods. However, it requires the conversion of seismic data to an incident angle gather. By contrast, analysis using coefficients of the amplitude polynomial is cost-effective because it allows examining amplitude variation with offset without involving the conversion process. However, it warrants further investigation into versatile application. The two different techniques can be complement each other effectively as AVO-analysis tools for the detection of hydrocarbon reservoirs.

Noise characteristics of a depolarized fiber-optic gyroscope incorporating single-mode fiber (단일모드 광섬유를 이용한 비편광 광섬유 자이로스코프의 잡음특성)

  • Jin, Young-Jun;Park, Tae-Yong;Park, Hee-Gap
    • Korean Journal of Optics and Photonics
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    • v.14 no.2
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    • pp.155-160
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    • 2003
  • We have constructed and characterized a depolarized fiber-optic gyroscope that uses a length of single-mode fiber as a sensing loop fiber. We have also calculated the noise characteristics of the gyroscope and have found an optimum phase modulation depth that gives the highest signal-to-noise ratio in the gyroscope. The random walk coefficient as small as 0.7$\times$10$^{-3}$ deg/√hr was obtained at the modulation depth of around 2.4 rad. The random walk coefficients measured at various modulation depths were found to be in reasonable agreement with the calculation.

Stability Analysis Using the Amplitude Envelope of Dynamic Pressure in the Rocket Combustor (로켓 연소기의 동압 진폭엔벨롭을 이용한 안정성 해석)

  • Lee, Soo Yong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.1
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    • pp.42-49
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    • 2021
  • As a measure of susceptibility on the combustion instability, thermo-acoustic instabilities in rocket combustion system was considered for the estimation of the operational stability margin. Growth rate, which governs the asymptotic stability behavior of the system, was determined from the dynamic data measured during combustion tests in order to understand the dynamic characteristics of combustor system. Frequency transform technique was first applied to determine the system parameters such as growth rate and/or damping coefficient for an interested mode from the time series pressure data, and the PDFs of pressure amplitude were extracted from the amplitude envelope of pressure oscillation for the stochastic analysis.

DESIGN OF A RISE TIME DISCRIMINATION CIRCUIT FOR X-RAY PROPORTIONAL COUNTER (X-선 비례계수관용 상승시간 선별회로 제작)

  • 남욱원;최철성
    • Journal of Astronomy and Space Sciences
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    • v.12 no.1
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    • pp.66-77
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    • 1995
  • It is possible to distinguish X-ray events from non X-ray events in proportional conters using the method of rise time discrimination (RTD). In order to subtract non X-ray background, we have developed a simple RTD circuit which will be applied to the proportional counter planned for a sounding rocket experiment. The entire circuit consists of two parts ; the rise time measurement circuit and the time to amplitude conversion circuit which includes the self-calibration mode. From the test with X-ray detecting system, we obtained that the background can be rejected more than 80% in the energy band 2∼12 keV. However we confirmed that the RDT method is not proper to be used for the energy range above 12kV.

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