• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 추계학술대회논문집
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• pp.881-885
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• 2002

This paper presents the performance and the algorithm of a 1/3-octave band spectrum control system. The system is developed to provide various spectrums in a high intensity acoustic chamber. The required spectrum, which usually comes from launch vehicle company, starts from 25Hz band and ends 10kHz band. Automatic spectrum control system is preferred since the system requires short settling time to guarantee the safety of test objects and to reduce the amount of operating gas. The developed system adapted a PCI data-acquisition/signal-generation board installed in a personal computer to implement whole control logic. The control software used three cascade digital Butterworth filters using software. The filers are designed following ANSI S1.11 standard to implement 1/3 octave band filter bank. The graphical user interface of the system guides the user to follow standard operation procedure. The averaged control spectrum showed less than 0.05 dB in every running 1/3-octave band.

• 한국음향학회지
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• 제14권1호
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• pp.108-114
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• 1995

입력단 또는 출력단이 원형 확장관 안으로 돌출되어 있는 소음기가 관내 전달 소음저감을 위해 많이 쓰이고 있다. 저주파수 영역에서의 소음저감 효과는 음파 진행 단면의 확장-축소와 입력단-출력단의 상대적 위치 등으로 발생되는 소음기의 리액티브 성분으로 설명이 된다. 본 연구에서는 입력 혹은 출력단에 동심으로 배치된 한개의 연장관이 단순 팽창형 소음기에 삽입되어 있는 경우에 대한 음향해석을 수행하였다. 해석방법으로는, 음장을 분리좌표계로 표현될 수 있는 몇개의 경계 표면으로 나누고, 각 표면에서의 음압 및 입자속도를 정규화된 음향 고유 모드로 전개하여 간단한 대수식으로 표현하였다. 제안된 해석적인 방법을 사용하여 소음기의 투과손실을 예측하였으며, 실험과도 잘 일치함을 관찰할 수 있었다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.1026-1031
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• 2003

A vibration isolation system fur a large reverberation chamber (1,228㎥, 1,000ton) has been installed. The reverberation chamber generates loud noise and induces high level of vibration to perform spacecraft acoustic environmental tests. The isolation system prevents vibration transfer from the chamber to enclosure buildings. This paper describes logical design process and commissioning experiments of the system. Design criteria have been induced from rigid body model of the chamber. Finite element model has been employed to select the characteristics of rubber pads. A total of 21 rubber pads have been installed between the chamber and supporting pedestals. A sand bag of 800kg was dropped on the chamber floor to measure the natural frequency of the isolation system. Absolute transmissibility has been measured while generating 145㏈ in the chamber. The natural frequency of the chamber is 10.5㎐, which is 80% of estimated value. Overall transmissibility at working frequency range (25㎐-10,000㎐) is less than -6㏈.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.869-872
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• 2005

The purpose of this study is on the prediction of the acoustic performance of the lined rectangular plenum chamber which can be used in the HVAC systems. The lined plenum chamber is modeled as a piston driven rectangular tube without mean flow and the acoustic pressure in the lined chamber is obtained by superposing the three dimensional pressure due to each of uniformly and harmonically fluctuating pistons. The arbitrary locations of inlet/outlet ports as well as the acoustic higher order modes generated at the area discontinuities of the port chamber interfaces are taken into consideration. The four-pole parameters can be derived by imposing the proper boundary conditions on each inlet and outlet ports. The lining material on the internal wall is assumed to be a bulk-reacting model. A single weak variation statement which satisfies the fluctuating rigid piston condition and the pressure and displacement continuity condition at the interface between the lining material and the airway was developed. The set of cosine functions were used as the admissible function when applying the Rayleigh-Ritz method. Computed results are compared with those predicted by using the locally-reacting lining material and experimental results, respectively. There are a good agreement shown between the results by the Rayleigh-Ritz method and the experiment results. The derived transfer matrices can be easily combined with other four-pole parameters of different types of mufflers for the calculation of the whole system performance.

• 한국항공우주학회지
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• 제31권6호
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• pp.79-87
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• 2003

로켓엔진에서 발생하는 고주파 연소 불안정(음향 불안정)을 억제하기 위해 엔진에 적용되는, 배플이나 음향공과 같은 연소 안정화기구를 설계하고 그 효과를 시험을 통해 검증하였다. 먼저, 음향 감쇠 관점에서, 선형 감쇠이론을 토대로 연소 안정화기구를 설계하였으며, 주요 설계인자로서 감쇠인자를 고려하여 여러 연소실에서의 감쇠인자를 수치적으로 계산하였따. 다음으로, 다양한 작동조건에서, 음향공이 장착된 무배플 연소실에서의 연소시험이 수행되었다. 이를 통해 무배플 연소실의 안정성 특성, 주요 유해주파수 및 유해 음향모드 등이 파악되었으며, 동적 안정성 여분이 상당히 작음이 확인되었다. 이는, 무배플 연소실의 연소 안정화에 현재 사양의 음향공의 효과가 미흡함을 입증한다. 배플의 효과를 입증하기 위해 배플장착 연소실에서 연소 안정성 평가시험을 수행하였고, 뚜렷한 연소 안정화 현상을 관측할 수 있었다. 이는 현 설계사양의 배플이 충분한 감쇠 효과를 가짐을 입증한다.

• 한국연소학회:학술대회논문집
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• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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• pp.145-152
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• 2003

The objective of the present study is to develop methodology for the assesment of combustion stability of liquid rocket injectors. To simulate actual combustion occurring inside of a thrust chamber, a full-scale injector has been employed in the study, which burns gaseous oxygen and mixture of methane and propane. The main idea of the experiment is that the mixing mechanism is considered as a dominant factor significantly affecting combustion instability in a full-scale thrust chamber. Single & multi split triplet injectors have been used with an open-end cylindrical combustion chamber. The characteristics revealed by excited dynamic pressures in gaseous combustion show degrees of relative acoustic damping depending on operating conditions. Upon test results, the direct comparison between various types of injectors can be realized for the selection of the best design among prospective injectors.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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• pp.229-234
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• 2004

The objective of the present study is to conduct model combustion tests for double swirl coaxial injectors to identify their combustion stability characteristics. Gaseous oxygen and mixture of methane and propane have been used as simulant propellants. Two model chambers tuned to the If acoustic resonance mode of a full-scale thrust chamber were manufactured to be used as a combustion cylinder. The main idea of the experiment is that the mixing mechanism is considered as a dominant factor significantly affecting combustion instability in a full-scale thrust chamber. Self-excited dynamic pressure values in a model chamber show different combustion stability zones with respect to a recess number. Upon test results, couplings between combustion conditions and the IT acoustic resonance mode become strengthened with the increase of a recess length.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 춘계학술대회논문집
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• pp.484-488
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• 2007

In this paper, the measurement system using the microphone array developed for analyzing cabin noise of the vehicle and its applications are discussed. The sensor is a three dimensional microphone array, the microphones and cameras are equipped on the rigid sphere. The cameras are used for acoustic visualization. As applications, the experiments in both reverberation chamber and anechoic chamber are discussed. These results show that this system is very useful to evaluate or improve the vehicle sound insulation performance.

• 소음진동
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• 제3권3호
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• pp.271-278
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• 1993

Acoustic characteristics of silencer system are affected by various geometric parameters such as cross sectional geometry, size of chamber, and location of inlet-outlet port. It is impossible to obtain exact solutions of the equations of acoustic wave propagation except few simple cases. So, we resort to numerical techniques to analyze performance of acoustic system. In this work, finite element formulation has been obtained to predict transmission loss of an arbitrary 3-dimensional muffler in the presence of mean flow of low mach number. The effect of the degree of the ellipticity of expansion chambers on the transmission loss has been studied using the resulting finite element equation.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.364-366
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• 2012

로켓 엔진의 연소실 내 음향학적 거동과 음향 감쇠 효과를 정량화하기 위한 방법을 연구하였다. DMD(Dynamic mode Decomposition) 방법을 이용한 결과와 기존의 정량화 방법인 damping factor를 이용해 구한 음향 감쇠 효과의 경향성을 배플 분사기가 장착된 연소실내의 음향 감쇠 정도를 비교 분석하여 나타내었다. 비교 결과, 기존의 정량화 방법과 DMD 방법을 이용해 구한 음향 감쇠 정도의 경향성이 일치하는 것을 확인하였다.