• 유체기계공업학회:학술대회논문집
• /
• 1998.02a
• /
• pp.150-156
• /
• 1998

가스터어빈 트랜지션 덕트 내에서의 공기 역학적인 거동을 입구 스월각의 변화에 대하여 고찰하였다. 트렌지션 덕트가 작은 확산각(divergence angle)을 가지더라도 스트럿 영향으로 인한 탈설계점에서의 유동 패턴은 트랜지션 덕트 내에서의 유동특성을 더욱 악화시킨다. 시험범위의 스월각은 마하수 변화에 따라 손실계수에 큰 영향을 주지 못하였으며 트랜지션 덕트 내에서의 손실 정조는 만족할만 하나, 시험결과에 따르면 저압터빈의 노즐손실은 큰 입사각의 영향으로 커질것으로 생각되며, 또한 스트럿으로부터 떨어져 나오는 와류는 저압터빈의 로우터 블레이드의 진동에 악영향을 미칠 것으로 생각된다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.14 no.1
• /
• pp.48-55
• /
• 2010

The purpose of this paper was to address the methodology of the air flow measurement using duct mach number that was considered area-weighed average obtained by total, static pressure and temperature measured at engine inlet duct. Without installing boundary rake, the prediction of air flow measurement was discussed. Actual air flow measurement and pressure value using pressure loss through inlet seal were described to improve the reliability and operability of altitude engine test facility.

• Aerospace Engineering and Technology
• /
• v.6 no.2
• /
• pp.29-34
• /
• 2007

The purpose of this paper was to address the methodology of the air flow measurement using duct mach number that was considered area-weighed average obtained by total pressure and temperature measured at engine inlet duct. Without installing boundary rake, the prediction of air flow measurement was discussed. Actual air flow measurement and pressure value using pressure loss through inlet seal were described to improve the reliability and operability of altitude engine test facility.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2006.05a
• /
• pp.1247-1251
• /
• 2006

공동주택의 보급 증가에 따라 화장실과 같이 환기용 덕트를 통한 층간 소음전달 문제가 예상되어 환기용 덕트에 간단히 설치하여 층간 소음 전달을 차단할 수 있는 환기장치용 소음기를 개발하였다. 본 개발품은 소음 차단 기능이 확실하고, 구조가 간단하며 분해조립이 가능하여 설치 및 유지보수가 용이한 제품이다. 또한 습기에 의한 부식이 없고, 먼지와 습기를 쉽게 제거할 수 있는 특징이 있다. 성능시험 결과 환기용 덕트를 통한 소음의 전달을 10dB 이상 저감시킬 수 있고, 삽입에 의한 압력손실 2mmAq 이하가 됨을 확인하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.04a
• /
• pp.144-152
• /
• 2011

In order to investigate the operation performance behaviors of the UAV's propulsion system to be operated long time in high altitude, the engine performance tests, which are simulated in the altitude engine test facility should be needed. If the test is performed in a existing altitude engine test facility, additional test apparatuses are required. Among them a proper design of the inlet and exhaust ducts that may directly affect the engine performance is very important. If the design is not adequate, the engine performance loss due to the flow behavior change and the pressure loss may be not similar to the real engine performance. In this work, firstly the engine inlet and exhaust ducts to be mounted to the existing altitude facility are modelled in 3D and its flow behaviors and pressure losses are analyzed using a commercial CFD tool, ANSYS's CFX, and the engine performance with the duct losses is calculated using the performance analysis program developed by C. Kong et al. Finally, the optimized inlet and exhaust ducts' configurations are proposed through the repeated analyses of various duct configurations.

• Journal of KSNVE
• /
• v.8 no.4
• /
• pp.733-740
• /
• 1998

본 논문은 덕트 내에 설치된 음향 스크린의 특성을 연구하였다. 다양한 형상의 음향 스크린의 투과 손실 측정을 통하여, 음향 스크린에 의해 생긴 두 개의 비대칭 경로가 특정 주파수에서 큰 협대역 소음 저감을 발생시킴을 알 수 있었다. 그리고, 실험과 수치적 모의 실험을 바탕으로 이러한 현상을 정확하게 설명할 수 있는 해석적 모델을 개발하였다.

• 월간 기계설비
• /
• s.9
• /
• pp.147-147
• /
• 1991

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.40 no.5
• /
• pp.497-503
• /
• 2016

In this study, we formulate an acoustical topology optimization problem to optimally design a partition layout inside the expansion chamber of a muffler. The lower-limit insertion loss value at a target frequency is constrained, and the partition volume is selected as an object function. In this study, we calculate the insertion loss outside the duct, while to determine the noise-attenuation performance, we use the insertion loss value calculated inside the duct or transmission loss value obtained in a previous study. We employ the finite-element model for acoustical analysis, and we determine the transmission of an incident acoustic wave through each finite element using the functions of design variables that change continuously between "0" and "1." The rigid body elements, which totally reflect incident waves, build up partitions. Finally, we compare optimal topologies that depend on the target frequency and the allowed lower-limit value of insertion loss.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2003.10a
• /
• pp.211-214
• /
• 2003

For prediction of the windmilling performance with consideration of bypass-duct loss of the twin-spool axi-centrifugal turbo-fan engine in flight condition, this study has examined the windmilling process and the physical phenomenon of the engine parts. Also, a mixing phenomenon with air passed through the bypass-duct has been analyzed. The results of the predicted windmilling performance has been compared and analyzed using the dimensional parameters.

• The Journal of the Acoustical Society of Korea
• /
• v.31 no.1
• /
• pp.11-18
• /
• 2012

In this paper, the occurrence of a stopband phenomenon when an acoustic wave propagates through periodically corrugated ducts is discussed using theoretical and BEM analyses. A 2-D duct with sinusoidally corrugated upper and lower walls is considered. When the magnitude of the sinusoidal corrugation is sufficiently small compared to the duct's height, the wave equation is solved with the multiple scaling perturbation method. Then stopbands for Bragg and non-Bragg resonances are computed from the condition where frequency becomes a complex number. A 2-D BEM analysis is performed to compute insertion loss of the duct, and stopbands are confirmed as predicted by analytical analysis.