• Title/Summary/Keyword: 주파수영역 해석

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Numerical Analyses on the Aerodynamic Characteristics of an Axial Type In-line Duct Fan (축류식 In-line duct fan의 공력특성에 관한 전산해석)

  • Cho, Lee-Sang;Ahn, Kwang-Weon;Cho, Jin-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.4
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    • pp.1-11
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    • 2004
  • Numerical analyses on the aerodynamic characteristics of a counter rotating axial flow fan were conducted for the development of an axial type in-line duct fan. The counter rotating fan has a front rotor and a rear rotor which are counter rotating each other. Blade design of the counter rotating fan was done by extension of design method for axial flow fan which consists of rotor and stator blades. Through flow analysis was performed using matrix method which is applied for flow fields prediction of compressors or turbines. Aerodynamic characteristics and characteristic curves of the counter rotating fan were analyzed by expansion of the frequency domain panel method with duct modeling. Pressure losses were higher at leading edge and hub region of rotor blades. Characteristic curve of the counter rotating fan was overpredicted without consideration of viscous effect.

The Analysis of Microwave Amplifier using an Extended FDTD Method (확장된 시간영역 유한차분법을 이용한 고주파 증폭기 해석)

  • 강희진;노범석;최재훈
    • Proceedings of the Korea Electromagnetic Engineering Society Conference
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    • 2000.11a
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    • pp.130-134
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    • 2000
  • 본 논문에서는 확장된 시간영역 유한차분법(Extended finite difference time domain method)을 이용하여 마이크로파 중폭기를 해석하였다. 회로에 포함되어 있는 능동 소자는 고주파 등가 회로를 이용하여 모델링 하였다. 고주파 등가 회로를 통하여 계산한 게어트와 드레인의 전류를 FDTD의 전계 계산식에 첨가향으로개 마이크로스트립 회로의 전자기파와 능동 소자와의 상호 작용을 특성 지었다. 해석 결과는 주파수 영역 회로 해석법(Frequency-domain circuit analysis)을 이용한 결과와의 비교를 통하여 정확성을 입증했다.

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State-Space Equation Model for Motion Analysis of Floating Structures Using System-Identification Methods (부유식 구조체 운동 해석을 위한 시스템 식별 방법을 이용한 상태공간방정식 모델)

  • Jun-Sik Seong;Wonsuk Park
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.37 no.2
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    • pp.85-93
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    • 2024
  • In this paper, we propose a method for establishing a state-space equation model for the motion analysis of floating structures subjected to wave loads, by applying system-identification techniques. Traditionally, the motion of floating structures has been analyzed in the time domain by integrating the Cummins equation over time, which utilizes a convolution integral term to account for the effects of the retardation function. State-space equation models have been studied as a way to efficiently solve floating-motion equations in the time domain. The proposed approach outlines a procedure to derive the target transfer function for the load-displacement input/output relationship in the frequency domain and subsequently determine the state-space equation that closely approximates it. To obtain the state-space equation, the method employs the N4SID system-identification method and an optimization approach that treats the coefficients of the numerator and denominator polynomials as design variables. To illustrate the effectiveness of the proposed method, we applied it to the analysis of a single-degree-of-freedom model and the motion of a six-degree-of-freedom barge. Our findings demonstrate that the presented state-space equation model aligns well with the existing analysis results in both the frequency and time domains. Notably, the method ensures computational accuracy in the time-domain analysis while significantly reducing the calculation time.

Verification of Frequency-Dependent Equivalent Linear Method (주파수 의존성을 고려한 등가선형해석기법의 검증)

  • Jeong, Chang-Gyun;Kwak, Dong-Yeop;Park, Du-Hee
    • Journal of the Korean Geotechnical Society
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    • v.24 no.12
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    • pp.113-120
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    • 2008
  • One-dimensional site response analysis is widely used to simulate the seismic site effects. The equivalent linear analysis, which is the most widely used type of site response analysis, is essentially a linear method. The method applies constant shear modulus and damping throughout the frequency range of the input motion, ignoring the dependence of the soil response on the loading frequency. A new type of equivalent linear analysis method that can simulate the frequency dependence of the soil behavior via frequency-strain curve was developed. Various forms of frequency-strain curves were proposed, and all curves were asserted to increase the accuracy of the solution. However, its validity has not been extensively proven and the effect of the shape of the frequency-strain curve is not known. This paper used two previously proposed frequency-strain curves and three additional curves developed in this study to evaluate the accuracy of the frequency-dependent equivalent linear method and the influence of the shape of the frequency-strain curves. In the evaluation, six recordings from three case histories were used. The results of the case study indicated that the shape of the frequency-strain curve has a dominant influence on the calculated response, and that the frequency dependent analysis can enhance the accuracy of the solution. However, a curve that results in the best match for all case histories did not exist and the optimum curve varied for each case. Since the optimum frequency-strain curve can not be defined, it is recommended that a suite of curves be used in the analysis.

Study on the Aeroservoelastic Stability Analysis with ZAERO (ZAERO를 활용한 서보공력탄성학적 안정성 해석기법 연구)

  • Rho, Hong-Gi;Bae, Jae-Sung;Hwang, Jai-Hyuk
    • Journal of Aerospace System Engineering
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    • v.14 no.5
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    • pp.1-8
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    • 2020
  • The aeroservoelastic analysis that deals with the interactions of the inertial, elastic, and aerodynamic forces and the influence of the control system have been performed. MSC Nastran was used for the free vibration analysis of the structure model as the pre-analysis. ZAERO was used to calculate the unsteady aerodynamic forces. The unsteady aerodynamic forces were verified by comparing with Doublet Hybrid Method. Karpel's Minimum-State Approximation method was used for approximation of the aerodynamic forces to the Laplace domain in the frequency domain. The aeroservoelastic state-space equation was obtained by combining the aeroelastic equation with the actuator dynamics. The analysis of aeroservoelastic stability concerning the elevator input of the high aspect ratio model was performed. The root-locus method and time-integration method were used for the analysis of aeroservoelastic in frequency and time domain.

Properties of Capacitance components depending on Frequency in Organic Light-Emitting Diodes by Temperatures (주파수 변화에 따른 유기발광소자의 온도별 용량성분 특성)

  • Ahn, Joon-Ho;Shin, Eun-Chul;Lee, Eun-Hye;Chung, Yong-Hwan;Jang, Kyung-Uk;Lee, Won-Jae;Seo, Dae-Shik;Kim, Tae-Wan
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2006.04a
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    • pp.76-77
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    • 2006
  • 유기발광소자의 주파수 응답 특성은 계면에서의 특성을 파악하는데 유요한 도구이다. 온 연구는 유기발광소자의 재료로 널리 알려진 $Alq_3$를 이용하여 소자를 제작한 후, 주파수 응답 특성을 이용하여 $Alq_3$의 등가회로를 해석하였다. 또 온도에 따른 용량성분을 분석하여 $Alq_3$에 인가된 전압에 따라 용량성분의 변화를 살펴보았다. 용량성분의 변화는 낮은 주파수 영역에서는 나타나지 않다가, 높은 주파수 영역에서 온도에 따라 미묘하게 감소하는 것을 볼 수 있다. 이는 낮은 주파수 영역에서 높은 주파수 영역으로 변화하면서 소자 내의 주된 성분이 저항성분에서 용량성분으로 변화하는 것을 의미하며 높은 주파수에서 온도에 따른 용량성분의 변화를 찾을 수 있었다.

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Acceleration-based Wireless Sensor Nodes Embedding Output-only Modal Analysis (모드해석 기법이 내장된 가속도기반 무선센서노드 개발)

  • Park, Jae-Hyung;Kim, Jeong-Tae;Ryu, Yeon-Sun;Yun, Chung-Bang
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2009.04a
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    • pp.10-13
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    • 2009
  • 본 논문에서는 모드해석 기법이 내장된 가속도기반 무선센서노드을 개발하였다. 이를 위해 다음과 같은 연구가 수행되었다. 첫째, 가속도 데이터를 취득하고 분석할 수 있는 가속도기반 무선센서노드를 설계하였다. 둘째, 무선센서노드를 이용한 구조건전성모니터링에 적합한 모드해석 기법으로 주파수영역분해법을 선정하였다. 셋째, 무선센서노드에서 모드해석을 독자적으로 수행하기 위한 분산 무선센서 네트워크기반 모드해석 알고리즘을 설계하고 무선센서노드에 내장하였다. 마지막으로, 개발된 무선센서노드를 PSC 거더모형에 설치하고 기존 구조건전성모니터링 시스템과의 성능비교를 통해 검증하였다.

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Aerodynamic Analysis of Counter-Rotating Propfans Around a Missile-Like-Body Using a Frequency Domain Panel Method (주파수영역 패널기법을 사용한 유도무기형태 동체에 장착된 엇회전식 프롭팬의 공력해석)

  • 조진수
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.6
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    • pp.1590-1597
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    • 1994
  • The aerodynamic analysis of a $6{\times}6$ counter-rotating propfan around a missile-like-body has been completed analytically using a frequency domain panel method. The present method requires Fourier transformation of flow field around the propfan in computing the velocities normal to the propfan lifting surfaces. The aerodynamic performance curve is determined by angle of attack and nonuniform inflow conditions. The inflow conditions result from the variations of missile flight speed, angle of attack, propfan location relative to control surfaces and control surface deflection angle. The two cases of propfan location relative to control surface, front and behind, are analyzed and the aerodynamic results are presented.

Dynamic Response Analysis of Tension Leg Platforms in Multi-directional Irregular Waves (Frequency Domain Analysis) (다방향 불규칙파중의 TLP의 동적응답해석 (주파수영역 해석))

  • 구자삼;조효제;이창호
    • Journal of Ocean Engineering and Technology
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    • v.8 no.1
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    • pp.23-32
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    • 1994
  • A numerical procedure is described for simultaneously predicting the motion and structural responses of tension leg platforms (TLPs) in multi-directional irregular waves. The developed numerical approach is based on a combination of a three dimensional source distribution method, the finite element method for structurally treating the space frame elements and a spectral analysis technique of directional waves. The spectral description for the linear responses of a structure in the frequency domain is sufficient to completely define the responses. This is because both the wave inputs and the responses are stationary Gaussian ran dom process of which the statistical properties in the amplitude domain are well known. The hydrodynamic interactions among TLP members, such as columns and pontoons, are included in the motion and structural analysis. The effect of wave directionality has been pointed out on the first order motion, tether forces and structural responses of a TLP in multi-directional irregular waves.

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The Study of the Sensorineural Hearing Loss Compensation Algorithm using Psychoacoustics Model (심리음향모델을 적용한 난청 보정 알고리즘의 연구)

  • 노형철;김헌중;한헌수;차형태
    • Proceedings of the IEEK Conference
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    • 2000.09a
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    • pp.189-192
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    • 2000
  • 본 논문에서는 청각 장애인의 보다 향상된 보청 환경을 조성하고자 청각손실을 심리음향 모델을 적용하여 감음 신경성 난청을 보정하는 알고리즘을 제안한다. 제안한 알고리즘에서는 난청의 유형은 내이에서부터 중추 뇌에 걸친 감음계와 신경계의 장애에서 비롯되는 감음신경성 난청(sensorineural hearing loss)으로 주파수 영역상에서 MTH(minimum hearing threshold)가 균일하지 않게 상승하게되어 가청영역이 좁아지는 문제점을 해결하기 위한 방법으로 각각의 주파수 밴드마다 멀티밴드 압축 알고리즘을 적용하였다. 그러나 이 경우 각각의 주파수 밴드에 따른 서로 다른 가청 영역의 영향에 의한 변형된 스펙트럼 모양으로 인해 spectral contrast reduction과 변형된 마스킹 특성으로 인해 음성 변별력에 제한을 가하게 된다. 이것은 주변 주파수 성분들에 의한 마스킹 효과에 의한 것으로, 신호에 대한 난청인이 느끼는 지각 영역(perceptual domain)에서의 해석과 심리음향 모델 파라미터를 통한 보청기의 개발이 이루어져야 하며, 본 논문에서 그 알고리즘을 적용하였다.

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