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음원 분포선 위치가 발사체 이륙 음향하중에 미치는 영향
이정권(Jeong-Guon Ih),최상현(Sang-Hyeon Choi),이익진(Ik-Jin Lee) 한국소음진동공학회 2015 한국소음진동공학회 학술대회논문집 Vol.2015 No.4
Intense acoustic load is generated when a launch vehicle lifts off, causing the damaging vibrations at the launch vehicle or satellite within the fairing. This paper is concerned with the prediction of lift-off acoustic loads for a launch vehicle. As a test example, the lift -off acoustic load on the Korean launch vehicle, NARO, is predicted by the existing calculation tool, the modified Eldred’s second method. Although the acoustic sources, assumed as point sources, are to be located along the center line of the exhaust plume in using the Eldred’s prediction method, the exact location of the deflected center line of exhaust gas flow is not usually known. To search for t he most appropriate source positions, six models of source line distribution are suggested and the acoustic load prediction results from these models are compared with the actual measurements. It is found that the prediction error for the Naro is the smallest when the centerline of the turbulent kinetic energy contour is used as the source line.
이준신,이정권,Lee, Jun-Shin,Lee, Jeong-Guon 한국음향학회 1995 韓國音響學會誌 Vol.14 No.1
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. Cylindrical chamber mufflers with an extended inlet or outlet are extensively used in many application fields to reduce the propagated noise in ducts. The basic attenuation effectivencess in the low frequency region can be explained by the reactive wave action inside the expansion chamber associated with the geometric configurations of the inlet and outlet locations, and the area expansion of the jacket. In this study, an acoustic analysis is carried out for a concentric extended pipe inserted into a simple expansion chamber. An algebraic equation is derived by using the eigenfuction expansion and orthogonality principle in which the acoustic pressures and particle velocities defined on each subdivided surface are expressed by the separable coordinates. By using the proposed analytical method, transmission losses are predicted for several configurations of the concentric extended systems and they agree very well with experimental results.