• 한국소음진동공학회논문집
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• 제15권6호
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• pp.687-696
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• 2005

Acoustic power spectrum of the upstream and downstream sound field due to an isotropic frozen turbulent gust impinging on a cascade of flat plate airfoils are computed by using a analytic formulation derived from Smith's method, and Whitehead's LINSUB codes. A parametric study of the effects on sound power of the number of blades and turbulence length scale is performed with an emphasis on analyzing the characteristics of sound power spectrum. Through the comparison of the computed results of sound power, it is found that acoustic power spectrum from the 2-D cascade subject to a ingested turbulence can be categorized into two distinct regions. one is lower frequency region where some spectral components of turbulence do not contribute to the cut-on acoustic modes and therefore the effect of the cascade geometry is more dominant ; the other is higher frequency region where all of spectral components of turbulence make contributions to cut-on acoustic modes and thus acoustic power is approximately proportional to the blade number.

• 한국산학기술학회논문지
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• 제15권7호
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• pp.4659-4664
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• 2014

산업 현장에서 발생하는 소음은 작업자의 건강과 작업 효율에도 영향을 줄 뿐 아니라, 주변의 주거지역의 소음 민원의 원인이 된다. 본 논문에서는 중소규모 공장에서 많이 사용되는 송풍기에서 발생하는 소음을 3차원 공간에서 능동소음제어기(ANC)를 이용하여 저감하는 기술 개발을 위한 기초 연구를 수행하였다. 이를 위해 ANC의 설정과 결과 데이터를 용이하게 파악할 수 있는 시뮬레이터 프로그램을 Labview를 이용하여 작성하여 음압레벨, 스펙트럼, 등가소음도 등의 데이터를 비교하였다. 소음 데이터는 현재 중소규모 공장에서 운전 중인 터보팬 송풍기에서 발생하는 소음을 기기 주변 17개의 위치에서 녹음하여 사용하였다. 모의실험 결과 17 지점 모두 500Hz 이하 저주파 대역에서 파워 스펙트럼이 최대 40dB 줄었으며 등가소음레벨이 평균 12.6dB 감쇄되는 결과를 보였다.

• 한국신뢰성학회지:신뢰성응용연구
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• 제7권2호
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• pp.89-100
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• 2007

For the certification of aircraft and part, it must be show the compliance with applicable requirements through system safety assessment. The safety assessment process should be planned and managed to provide the necessary assurance that all relevant failure conditions have been identified and that all significant combinations of failures which could cause those failure conditions have been considered. Complex systems, especially aircraft, should take into account any additional complexities and interdependencies which arise due to integration. In all cases involving integrated systems, the safety assessment process is of fundamental importance in establishing appropriate safety objectives for the system and determining that the implementation satisfies these objectives. This study review the safety assessment for the certification process of the aircraft engine system and analyze turbo-fan engine by fault analysis method for compliance with airworthiness requirement of aircraft engine system.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.1007-1010
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• 2006

In order to optimize the rotating angle of the auto louver, the air-cleaner with turbo fan was numerical and experimentally analyzed . The noise generated from the auto louver was changed by modifying the installation angle of the louver. Flow field and flow noise were analyzed numerically by commercial tool SC/Tetra and FlowNoise S/W. Experiment was also done at anechoic chamber. From the numerical and experimental data, we can find the optimal rotating angle for auto louver of the air-cleaner.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 춘계학술대회논문집
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• pp.1140-1145
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• 2003

In this paper, some dominant aeroacoustic characteristics of fans used in appliances are reviewed. The numerical attempts to analyze tile aeroacoustic noise of fans are briefly reviewed for various fans. Axial fans for refrigerator, cross flow fans fer air-conditioner, sirocco fans and turbo fans are anal: zed. The unsteady flow field, which is essential data for aeroacoustic analysis, is calculated by commercial CFD code. Acoustic pressure is calculated by Ffowcs Williams and Hawkings equation and Lowson's equation. During the analysis, dominant noise sources are identified.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.592-596
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• 2012

항공기 성능해석을 하기 위해서는 엔진 상세 데이터가 필수적으로 요구된다. 하지만 이러한 엔진 상세 데이터는 항공회사의 경험으로 축적된 자산이기 때문에 엔진 성능 정보를 구하기 어렵다. 본 연구에서는 일반적으로 공개된 자료와 문헌정보를 이용하여 혼합흐름 터보팬 엔진 성능 모델을 구축하고 결과를 비교하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.101-104
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• 2010

최근 무인기 혹은 소형 항공기들에 대한 수요가 증가함에 따라 소형 터보제트 혹은 터보팬 엔진의 수요가 꾸준히 증가하고 있다. 이러한 소형 엔진은 요구 추력을 달성하면서 크기와 무게를 줄이는 것이 가장 중요한 설계 인자인데, 이는 곧 비추력(Thrust to Weight) 값이 매우 높음을 의미한다. 비추력 값이 높은 엔진을 설계하기 위해서, 압축기 혹은 터빈 등의 핵심구성품의 경우 크기를 줄이고 단수를 줄이는 방법이 가장 효과적이다. 특히 축류압축기의 경우 일반적으로 다단으로 구성하는데 여러 단으로 구성된 압축기 중에서 단수를 줄이고 남은 단에서의 압력비를 높이는 '고부하 압축기'를 채용함으로써 이러한 문제를 해결할 수 있다. 최근 국내에서도 축류형 압축기에 대한 개발의 필요성이 꾸준히 제기되고 있으며, 이에 본 논문에서는 고부하 축류형 압축기의 설계 및 성능 리뷰 중 주요한 사항에 대해 소개하고자 한다.

• 한국소음진동공학회논문집
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• 제15권10호
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• pp.1177-1185
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• 2005

This paper investigates the noise radiated by a cascade of flat-plate airfoils interacting with homogeneous, isotropic turbulence. At frequencies above the critical frequency, all wavenumber components of turbulence excite propagating cascade modes, and cascade effects are shown to be relatively weak. In this frequency range, acoustic power was shown to be approximately proportional to the number of blades. Based on this finding at high frequencies, an approximate expression is derived for the power spectrum that is valid above the critical frequency and which is in excellent agreement with the exact expression for the broadband power spectrum. The approximate expression shows explicitly that the acoustic Power above the critical frequency is proportional to the blade number, independent of the solidity, and varies with frequency as ${\phi}_{ww}(\omega/W$), where ${\phi}_{ww}$ is the wavenumber spectrum of the turbulence velocity and W is mean-flow speed. The formulation is used to perform a parametric study on the effects on the power spectrum of the blade number stagger angle, gap-chord ratio and Mach number. The theory is also shown to provide a close fit to the measured spectrum of rotor-stator interaction when the mean square turbulence velocity and length-scale are chosen appropriately.

• 한국소음진동공학회논문집
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• 제23권9호
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• pp.841-849
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• 2013

Workers engaged in construction works have been exposed to high levels of noise during their work in tunnels. Noise is one of the major health hazards for employees working in construction sites. The aim of this study is to evaluate the noise levels generating from tunneling equipments such as jumbo drills, backhoes, payloaders, shotcrete machines and service cars. Explosion and turbo fan noises were also monitored. A high precision sound level meter was introduced for measuring LAeq, LAFmax, LAFmin and LCpeak noises in 5 tunneling work sites that were located in Seoul, Kyunggi-do and Kangwon-do areas with NATM and shield methods. The highest noise was recorded by explosion(151.9 dB LCpeak) followed by jumbo drills of higher than 110 dB(A) LAeq. Backhoe normally generated 90~110 dB(A) LAeq while breaking work of rock showed additional around 5~15 dB(A). Noise exposure levels for payloader and shotcrete machine scored more than 90 dB(A) which might be a source of noise-induced hearing loss. Additional research in revealing noise levels from construction equipments operating in tunneling works may enhance the protection of workers who exposed to noise primarily at the sites.

• 한국소음진동공학회논문집
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• 제16권3호
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• pp.263-269
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• 2006

The objective of the present work is to develop a time-domain numerical method of broadband noise in a cascade of airfoils. This paper focuses on dipolar broadband noise sources, resulting from the interaction of turbulent inflows with the flat-plate airfoil cascade. The turbulence response of a two-dimensional cascade is studied by solving both of the linearised and the full nonlinear Euler equations employing accurate higher order spatial differencing, time stepping techniques and non-reflecting inflow/outflow boundary condition. The time-domain result using the linearised Euler equations shows good agreement with the analytical solution using the modified LINSUB code. Through the comparison of the nonlinear time-domain result using the full nonlinear Euler equations with the linear, it is found that the acoustic mode amplitude of the nonlinear response is less than that of the linear response due to the energy cascade from low frequency components to the high frequency ones. Considering the merits of the time-domain methods over the typical time-linearised frequency-domain analysis, the current method is expected to be promising tools for analyzing the effects of the airfoil shapes, non-uniform background flow, linear-nonliear regimes on the broadband noise due to turbulence-cascade interaction.