• Title/Summary/Keyword: 소음 방향성

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Asymmetric Directionality of Broadband Ship Radiation Noise at Bow-Stern Aspect (광대역 선박방사소음의 선수-선미 비대칭 방향성)

  • Lee, Keunhwa;Kim, Minkyu;Seong, Woojae
    • The Journal of the Acoustical Society of Korea
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    • v.34 no.5
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    • pp.343-350
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    • 2015
  • In this paper, we perform a study on the directionality of broadband ship radiation noise, mainly resulting from propeller cavitation. By examining a few foreign studies for ship radiation noise and domestic data measured in Korean waters, it is reconfirmed that the asymmetric directionality of the ship radiation noise at bow and stern aspect is observed commonly. In order to explore the reason of this asymmetric directionality, a numerical analysis, based on the acoustic boundary element method, is applied into the geometric form equal to the commercial ship used in the domestic experiment. The numerical result demonstrates that the diffraction of the propeller cavitation noise by ship is a primary cause of the bow-stern asymmetry in the directionality of ship radiation noise.

Analysis on Acoustic Noise around Launch Pad Induced by the Launch of a Space Launch Vehicle (우주발사체 발사에 의한 발사장 주변의 음향 소음 분석)

  • Sim, Hyung-Seok;Choi, Kyu-Sung;Ko, Jeong-Hwan;Roh, Woong-Rae
    • Aerospace Engineering and Technology
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    • v.11 no.2
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    • pp.208-215
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    • 2012
  • The acoustic noise around a launch pad by launches of space launch vehicles was analyzed. The magnitudes of sound noise at some points near launch pad were predicted by locating the sound source at the exhaust jet plume of the rocket engine and considering several factors such as the directivity of the sound propagation and atmospheric attenuation. Specifically, the launch noise of Korea Space Launch Vehicle-I (KSLV-I) was estimated, and was compared to the actual measurement results. The analysis results proved to be heavily affected by the characteristics of directivity of sound propagation and the analysis showed good agreements with the measurements when the directivity of the sound was appropriately adjusted.

The Improvement of privately telephonic communication for cellular phone by acoustic approach (음향학적 접근에 의한 휴대 전화의 속삭임 통화 기능 향상)

  • Choi Sungjoon;Moon Wonkyu;Lee Jounghyun
    • Proceedings of the Acoustical Society of Korea Conference
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    • autumn
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    • pp.317-322
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    • 2001
  • 정보 통신 기술의 발달이 인간 생활에 많은 편리함을 가져다 주었지만 개인의 정보 유출이나 소음 공해 등의 여러 가지 문제점도 야기 시켰다. 특히 휴대 전화 통화시 사용자의 개인적인 정보들이 공공 장소에서 그대로 노출이 되고, 또 그러한 통화로 인해서 타인에게 소음 피해를 주기도 한다. 이러한 병폐를 막기 위해서 휴대 전화 사용자는 최대한 작은 소리로 통화를 하되, 상대방에게 의도하고자 하는 바를 확실히 전달하여야 한다. 그러기 위해서는 휴대 전화에 근접 통화가 가능해야 하며, 일정한 방향의 방향성을 가져서 주위의 잡음에 대해 독립적으로 작동하도록 해야한다. 본 논문에서는 이러한 기능을 향상시키기 위하여 음향학적 이론을 바탕으로 휴대전화에 사용되어지는 마이크로폰을 새로 설계, 제작하고 그 성능을 시험하였다. 아주 작은 소리로 근접 통화를 할 때 발생하는 팝핑(popping) 현상이 최소한이 되도록 미세관 배열을 적용하였으며, 외부 소음 영향을 줄이기 위하여 방향성을 증폭시키고자 음원의 위치에 초점을 맞추는 기술을 적용하였다. 방향성 증폭은 4개의 마이크로폰 사용과 근거리 음원의 방향성 증가를 위한 신호 처리기술을 적용하였다. 이 기술의 적용 효과를 실험을 통하여 검증할 수 있었다.

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Array gain estimated by spatial coherence in noise fields (소음 환경에서 공간상관성을 이용한 배열이득 추정)

  • Park, Ji Sung;Choi, Yong Wha;Kim, Jea Soo;Cho, Sungho;Park, Jung Soo
    • The Journal of the Acoustical Society of Korea
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    • v.35 no.6
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    • pp.427-435
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    • 2016
  • Array Gain (AG) is a metric to measure the performance of an array of acoustic sensors. AG is affected by the configuration of array, frequency and array element spacing, and the directivity of the ambient noise. In this paper, an algorithm to calculate AG based on the spatial coherence is used, and the results are verified through sea-going experiment. The method using the spatial coherence can be used to consider the arbitrary shape of an array and directionality of ambient noise. In the sea-going experiment, the towed source was used to transmit the Continuous Wave (CW), and was received at the horizontal line array on the seabed. The ambient noise was measured between the source transmission. The experimental AG was calculated from the SNR (Signal to Noise Ratio) of single sensor and an array of sensors. Finally, the predicted AG is shown to agree with the experimental value of AG.

Adaptive Beamforming Applied to Bearing Estimation of DIFAR Signal with Highly Directional Noise (높은 방향성 소음환경에서 DIFAR 수신센서 신호의 적응 빔형성에 의한 방위추정)

  • Shin, Kee-Cheol;Kim, Jea-Soo
    • The Journal of the Acoustical Society of Korea
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    • v.30 no.8
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    • pp.474-481
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    • 2011
  • Conventional beamforming is ineffective in producing directional information in system with sparse degree of the freedom such as DIFAR (DIrectional Frequency Analysis and Recording) sonobuoy and in the presence of high directional noise. In this paper, Adaptive beamforming techniques are applied to produce directional spectra from a small number of sensors in highly directional noise environment. Conventional method as well as minimum variance and eigenvectors as adaptive method are evaluated via numerical test and real data.

Directional Harmonic Wavelet Analysis (방향성 조화 웨이블렛 해석 기법)

  • 한윤식;이종원
    • Journal of KSNVE
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    • v.8 no.5
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    • pp.957-963
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    • 1998
  • A new signal processing technique, the directional harmonic wavelet map(dHWM), is presented to characterize the instantaneous planar motion of a measurement point in a structure from its transient complex-valued vibration signal. It is proven that the directional auto-HWM essentially tracks the shape and directively of the instantaneous planar motion, whereas the phase of the directional cross-HWM indicates its inclination angle. Finally, the technique is suessfully applied to an automobile engine for characterization of its transient motion during crank-on/idling/engine-off.

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Development of a Helicopter Rotor Test Rig and Measurement of Aeroacoustic Characteristics (헬리콥터 로터 시험장치의 개발 및 공력소음특성의 측정)

  • Rhee, Wook;Choi, Jong-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.3
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    • pp.10-16
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    • 2004
  • In this paper the aeroacoustic characteristics of a helicopter main rotor system is measured by using a pair of scaled rotor blades. A low noise rotor test jig is developed for noise measurement and the rotational speed, thrust and torque are measured simultaneously in order to match the aerodynamic conditions with the full scale rotor. The accuracy of the force measurement device was checked through a calibration procedure. The measured thurst and torque with a 1.2m rotor are compared to the results of analytical prediction and showed that the thrust data at various rotational speed followed the prediction relatively well, but the torque data considered less accurate. It is also found that the background noise level of the test rig is sufficiently low, and the measured noise level from the rotor can be scaled with rotor tip speed. However, the Mach number dependancy and the directivity changes depend on the noise source characteristics.