• Proceedings of the Acoustical Society of Korea Conference
• /
• 1998.06e
• /
• pp.49-52
• /
• 1998

콘서트홀의 음향상태를 평가하기 위해서는 설문지를 통하여 주관적인 선호도를 조사하는 방법과 측정을 통하여 객관적인 지표를 뽑아내는 방법이 있다. 콘서트홀의 음향특성에 영향을 주는 가장 중요한 객관적 지표로서는 친밀도, 공간감, 잔향시간, 명료도, 음의 따뜻함, 라우드니스 등을 들 수가 있다. 국내에서 가장 대표적인 콘서트홀이라고 할 수 있는 예술의 전당 음악당에 대해서 위의 개관적 지표 중 5가지 요소를 실제 측정을 통해 추출하였다. 그 결과 예술의 전당 음악당은 친밀도와 공간감 면에서 조금 부족한 면을 보여 주었고 나머지 3가지 요소에 있어서는 클래식 연주에 적합한 콘서트홀로서의 결과를 보여 주었다. 공간감과 친밀도를 향상시키기 위해서는 음악당 천장에 반사판을 설치하는 것이 필요하다고 사료된다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2007.04a
• /
• pp.13-16
• /
• 2007

Nonlinear acoustic damping of a half-wave acoustic resonator in a combustion chamber is investigated numerically. First, in a baseline chamber without any resonators, acoustic behavior is investigated over the wide range of acoustic amplitude from 80 dB to 150 dB. Decay rate increases nonlinearly with acoustic amplitude and nonlinearity becomes appreciable at acoustic amplitude above 125 dB. Next, damping effect of a half-wave resonator is investigated. Nonlinear acoustic excitation does not affect optimum tuning condition of the resonator, which is derived from linear acoustics. A half-wave resonator is effective even for acoustic damping of high-amplitude pressure oscillation, but its function of acoustic damper is relatively weakened compared with the case of linear acoustic excitation.

• The Journal of the Acoustical Society of Korea
• /
• v.42 no.3
• /
• pp.189-202
• /
• 2023

In this study, the acoustic performance was analyzed by architectural shapes of the hall. There are four architectural shapes of halls. They are rectangular, horseshoe, surround, and fan-shape. Eight acoustic parameters were used to determine the acoustic performance. These are RT₆₀, EDT, C₈₀, BQI, LF, G_mid, G₁₂₅ and ITDG. First, measurement data of famous concert halls around the world were analyzed. The correlation coefficient R was obtained by regression analysis of the relationship between the subjective ranking of the halls and the acoustic parameters. It was found that BQI, G, and ITDG have higher correlation coefficients R. Also the average of acoustic parameters for each architectural shape were obtained. The total acoustic performance for each shape was calculated by using the correlation coefficient R as a weight for each acoustic parameters. As a result, rectangular halls and horseshoe halls showed good acoustical performances. Second, 3D models of each architectural shape were created and acoustic simulation had been performed. The simulation was performed by creating 3D models of each four shapes of concert halls with the same volume and sound absorption coefficient. Listening test was carried out using the sound source which is created from impulse responses of 3D model. As a result, rectangular hall and horseshoe hall showed the best performance however surround hall and fan-shaped hall showed relatively poor performance.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2008.04a
• /
• pp.272-275
• /
• 2008

공연장음향성능에 영향을 미치는 중요한 부자재중의 하나인 음향반사판의 면밀도 변화에 따른 흡음특성 변화를 조사하였다. 음향반사판은 목질계반사판으로 밀도 변화는 $11\;㎏/m^2{\sim}41k\;㎏/m^2$으로 총 3개의 시료를 대상으로 측정하였다. 저주파 대역에서의 흡음률을 측정하기 위하여 서브우퍼와 무지향성 스피커를 사용하였으며 측정결과 중고주파수 대역의 흡음률은 면밀도 변화에 따라 큰 차이가 없었으나 저주파수 대역의 흡음률을 면밀도 변화에 따라 차이가 있는 것으로 나타났다. 향후 음악 공연 공간내의 음향반사판의 면밀도 변화에 따른 실내 음향 특성 변화 및 설계지침에 대한 연구가 필요할 것으로 사료된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.30 no.4
• /
• pp.28-37
• /
• 2002

Acoustic behavior in combustion chamber with acoustoc cavity is numerically investigated by adopting linear acoustic analysis. Helmholtz-type resonator is employed as a cavity model to suppress acoustic instability passively. The tuning frequency of acoustic cavity is adjusted by varying the sound speed in acoustic cavity. Through harmonic analysis, acoustic pressure responses of chamber to acoustic oscillating excitation are shown and the resonant acoustic modes are identified. Acoustic damping effect of acoustic cavity is quantified by damping factor. As the tuning frequency approaches the target frequency of the resonant mode to be suppressed, mode split from the original resonant mode to lower and upper modes appears and thereby damping effect is degraded significantly. Considering mode split and damping effect as a function of tuning frequency, it is desirable to make acoustic cavity tuned to maximum frequency of those of the possible splitted upper modes.

• Proceedings of the Korean Society of Fisheries Technology Conference
• /
• 2003.05a
• /
• pp.74-75
• /
• 2003

인공어초를 투입한 후 그 효과를 조사하는 수단으로는 자망 등에 의한 어획실험, 잠수조사, 표지방류 등이 있다. 이러한 방법들은 이동중인 어류의 생태를 파악하는데는 부족한 점이 많다. 따라서 이동 중인 어류에 초음파 핑거를 부착해 추적하는 방법이 어류의 생태 조사에 많이 이용되고 있다. 본 연구에서는 통영바다목장에 방류한 어류의 이동범위 및 일주행동을 측정하기 위하여 장기선 음향텔레베트리 기법을 사용하여 2003년 3월 20일부터 3월 26일까지 통영바다목장 해역에서 실험을 행하였다. (중략)

• The Journal of the Acoustical Society of Korea
• /
• v.21 no.8
• /
• pp.708-718
• /
• 2002

In this paper, the problems in identifying the noise sources by using the sound intensity technique are dealt with for the general radiated near-field from vibro-acoustic sources. For this purpose, a three-dimensional model structure resembling the engine room of a car or heavy equipment is considered. Similar to the practical situations, the model contains many mutually coherent and incoherent noise sources distributed on the complicated surfaces. The sources are located on the narrow, connected, reflecting planes constructed with rigid boxes, of which a small clearance exists between the whole box structure and the reflecting bottom. The acoustic boundary element method is employed to calculate the acoustic intensity at the near-field surfaces and interior spaces. The effects of relative source phases, frequencies, and locations are investigated, from which the results are illustrated by the contour map, vector plot, and energy streamlines. It is clearly observed that the application of sound intensity technique to the reactive or reverberant field, e.g., scanning over the upper engine room as is usually practiced, can yield the detection of fake sources. For the precise result for such a field, the field reactivity should be checked a priori and the proper effort should be directed to reduce or improve the reactivity of sound field.

• Survey Research
• /
• v.11 no.2
• /
• pp.29-44
• /
• 2010

The aim of this study was to determine principal non-acoustical factors for noise annoyance in the vicinity of Kimpo Airport in Seoul, Korea. Noise annoyance was estimated using self-reported annoyance scale. We have conducted a social survey aiming to identify the main sound sources, evaluate the annoyance and analyse the main effects of noise on people. Acoustical and non-acoustical variables are expected to greatly affect annoyance responses. This study divided acoustical variables into aircraft, road traffic and neighboring noises, and non-acoustical variables into demographic, situational and attitudinal variables. The study performed multiple regression analysis to determine the influences each variable has on annoyance responses. Acoustical variables affect noise annoyance to aircraft and neighboring noise except road traffic noise. For road traffic and neighboring noise annoyance was affected by non-acoustical variable, insulation by housing type. For aircraft noise, main noise source of this area, annoyance was affected by acoustical variable and some non-acoustical variables, mainly exposure time.

• 한국지구물리탐사학회:학술대회논문집
• /
• 2008.10a
• /
• pp.185-190
• /
• 2008

Geophysical survey were investigated in the offshore around East Sea Research Institute, Korea Ocean Research and Development Institute (Jukbyeon-myun, Uljin-gu, Gyeongsangbuk-do, Korea). The surveys were conducted aboard the R/V Jangmok in 2008 using a hull-mounted EM 3002 multi-beam echosounder. Precise bathymetry and seabed images were obtained using multi-beam and thicknesses of sedimentary layer were found through seismic survey. Submarine topography deepens parallel to the coastline to -60 m and rock mass distributed in the southeast of study area. By finding the thickness of sedimentary layer through seismic survey, a sedimentary thickness on the study area was established. Futhermore, monitoring data of bathymetry, substructure and sedimentary environment will be secured through successive geophysical investigation.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.11 no.3
• /
• pp.35-42
• /
• 2007

Acoustic damping induced by gap width between baffled injectors is investigated numerically, which are installed to suppress pressure oscillations in a model rocket combustor. The previous work reported that the baffled injectors show larger acoustic damping with the gap width between injectors. It is simulated numerically and its mechanism is examined. Damping factors are calculated as a function of gap width and it is found that the optimum gap is 0.1 mm or so. For understanding of the improved damping induced by the gap, dissipation rate of turbulent kinetic energy and vorticity are calculated as a function of the gap. Both parameters have their maximum values at the specific gap and especially, the dissipation rate has the same profile as that of damping factor. It verifies that the improved damping made by the gap is attributed to the increased acoustic-energy dissipation.