• 한국신재생에너지학회:학술대회논문집
• /
• 2009.06a
• /
• pp.508-511
• /
• 2009

풍력터빈 블레이드에서 발생하는 공력소음원의 위치 특성을 파악하기 위해 마이크로폰 어레이를 사용하여 소음원 풍동시험을 수행하였다. 풍동시험은 KARI 중형 아음속풍동에서 수행되었으며, 소음원의 위치파악을 위해 시간영역 회전체 빔포밍기법을 사용하였다. 기존 시간영역 회전체 빔포밍 기법의 경우 시험데이터 해석에 많은 시간이 소요되나, 본 논문에서는 원통형 좌표계에서 회전각 격자간격과 해석기간 간격 사이의 상관조건을 도입하여 데이터 해석시간을 기존 방법 대비 1/5로 단축하였다. 시험결과 나타난 주파수에 따른 블레이드 공력소음원의 위치 특성은 2kHz 이하 대역에서는 블레이드 반경 80% 부근에 주소음원이 위치하며, 4kHz 이상 대역에서는 블레이드 끝단 부근에 주 소음원이 위치하고 있다.

• Aerospace Engineering and Technology
• /
• v.3 no.1
• /
• pp.45-55
• /
• 2004

In this study, a time marching free wake method was used for the aerodynamic analysis and the boundary element method was used for the aeroacoustic analysis of the Tail Fan, respectively. In addition, variations of blades position in duct were performed and the aeroacoustic analysis shows a marginal improvement in noise level.

• Journal of the Korean Society for Railway
• /
• v.10 no.6
• /
• pp.786-791
• /
• 2007

Aerodynamically generated noise is dominant when the train speed approaches 300km/h. This noise sources is caused by the turbulent flow separations or vortex shedding from the train structure. Experiments were performed to investigate the characteristics of aerodynamic noise sources generated from exterior of the KTX trains and HSR-350x, especially from the inter-coach spacing. Measurements of both the inside and outside of the cabin are carried out to investigate the characteristics of the noise. Effect of the size of the mud-flap has been investigated through an wind tunnel test and it has been found that the low frequency noise is strongly dependent on the size of the gap. Also performed is an array measurement to locate different noise sources from the high-speed train. spectral characteristics of exterior noise sources are examined.

• The Journal of the Acoustical Society of Korea
• /
• v.43 no.1
• /
• pp.131-137
• /
• 2024

Aerodynamic noise generated by the surrounding flow of a train traveling at high speed affects both outdoor and indoor noise. This study's goal is to develop a test method to measure and quantitatively evaluate aerodynamic noise through pressure perturbation data on the train surface. To accurately evaluate aerodynamic noise, it is important to separate and evaluate the compressive and incompressible pressure fluctuations mixed in the acquired surface pressure fluctuation data. This is because the noise transmission characteristics of the two pressure fluctuations are different. First, the installation length and interval of the microphone were determined to acquire surface pressure fluctuation data, and wavenumber-frequency analysis was performed to separate incompressible pressure fluctuation and compressible pressure fluctuation to obtain a sound pressure level spectrum. Finally, as a result of comparing the test results measured in the train head and trail, It was confirmed that the pressure fluctuation on the train head surface was greater than that on the tail.

• Journal of KSNVE
• /
• v.3 no.2
• /
• pp.95-102
• /
• 1993

고속철도를 포함한 철도운행에 있어서 소음문제는 중요한 환경문제의 하나 이다. 지금까지 철도소음에 관한 국내에서의 연구는 철도소음 기준과 관련된 일부 연구를 제외하고는 거의 없는 상황이다. 앞으로 고속철도의 성공적인 운행을 위하 여는 선로변에서의 소음저감 대책으로 지형과 궤도조건에 따른 소음피해 예측과 소음원 특성을 고려한 효과적인 방음설계에 대한 연구가 필요하다. 또한 경부고속 철도 노선에 터널이 많으므로 터널 미기압파의 발생과 그대책에 대한 연구가 필요할 것으로 생각된다. 이와 더불어 국산화 차량 개발을 위하여 차체와 판토그래프에서의 공력소음감소를 위한 공력해석, 전동소음과 구조물 소음 감소를 위한 차륜과 쾌도의 개선, 추진장치와 보조장치의 소음제어설계 등 각각의 소음발생원에 대한 이해와 소음저감 기술의 개발이 필요하다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 1997.04a
• /
• pp.573-580
• /
• 1997

본 고에서는 공력음향학에 대한 여러 분야 중에서 최근 국내에서 관심 있게 연구되어온 분야에 대하여 그 연구 내용과 연구 방법 등을 소개하고자 한다. 먼저 전형적인 유체의 소음원에 대해서 설명하고, 이에 대한 수치적 해석방법과 무향풍동을 이용한 실험, 그리고 본 음향학 이론에 대한 응용 사례들에 대해서 간략히 소개하고자 한다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2004.11a
• /
• pp.561-564
• /
• 2004

Acoustic holography is applied to automobile aeroacoustic noise. Automobile aeroacoustic noise has low coherence due to multiple independent sources and measurement noise. This paper discusses the reliability of acoustic holography on this low coherence condition. Main subjects are the number and position of reference microphones, which is used for a step-by-step scanning method, and measurement noise. A real automobile experiment verifies the results.

• Journal of Aerospace System Engineering
• /
• v.17 no.2
• /
• pp.26-37
• /
• 2023

Urban air mobility (UAM) is being developed as part of the next-generation aircraft, which could be a viable solution to entrenched problems of urban traffic congestion and environmental pollution. A new airport platform called vertiport as a space where UAM can take off and land vertically is also being introduced. Noise regulations for UAM will be strict due to its operation in a highly populated urban area. Ground effects caused by vertiport can directly affect aerodynamic forces and noise characteristics of UAM. In this study, ground effects of vertiport on aerodynamic loads, vorticity field, and far-field noise were analyzed using Lattice-Boltzmann Method (LBM) simulation and Ffowcs Williams and Hawkings (FW-H) acoustic analogy with a permeable surface method.

• 한국전산유체공학회:학술대회논문집
• /
• 2009.04a
• /
• pp.70-74
• /
• 2009

The helicopter development technology is improved by the increasing of computing power and advanced test facilities. The increasing efficiency of fuel consuming by the developing of improved lift-to-drag rotor system is the major issue, the noise reduction for ecology(civil area) and increase of survivability to reduce noise detection(battlefield) also are important. This investigation shows the helicopter external noise flight test methods, conventional military helicopter's(UH-60) experimental results and the numerical modeling method for aero-acoustic of rotor blade and the result of CAA(Computational Aero-Acoustic) for main rotor blade.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2011.04a
• /
• pp.492-497
• /
• 2011

Helicopter uses a rotor system to generate lift, thrust and forces, and its aerodynamic environment is generally complex. Unsteady aerodynamic environment arises such as blade vortex interaction. This unsteady aerodynamic environment induces vibratory aerodynamic loads and high aeroacoustic noise. Those are at N times the rotor blade revolutions (N/rev). But conventional rotor control system composed of pitch links and swash plate is not capable of adjusting such vibratory loads because its control is restricted to 1/rev. Many active control methodologies have been examined to alleviate the problem. The blade using active control device manipulates the blade pitch angle at arbitrary frequencies. In this paper, Active Trailing-edge Flap blade, which is one of the active control methods, is designed to modify the unsteady aerodynamic loads. Active Trailing-edge Flap blade uses a trailing edge flap manipulated by an actuator to change camber of the airfoil. Piezoelectric actuators are installed inside the blade to manipulate the trailing edge flap.