• 설비공학논문집
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• 제15권3호
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• pp.177-186
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• 2003

In the present study, the flow characteristics of developing turbulent flows are investigated at the exit region of a square cross-sectional 180" curved duct with dimensions of 40mm$\times$40mm$\times$4000mm (height $\times$ width $\times$length). Smoke particles produced from mosquito coils were used as seed particles for the LDV measurement. Experiments were carried out to measure axial velocity profiles, shear stress distributions and entrance lengths by using an LDV system and Rotating Machinery Resolver RMR with PHASE software. Experimental results clearly show that the time-averaged Reynolds number does not affect oscillatory flow characteristics because the turbulent components tend to balance the oscillatory components in the fully developed flow region. Also, the velocity profiles are in good agreement with 1/7power law such as the results of steady turbulent flows. The turbulent intensity linearly increases along the walls and is slightly higher, especially in the period of deceleration. On the other hand, the LDV measurements show that shear stress values in slightly higher in the period of deceleration due to the flow characteristics in the exit region. The entrance length where flows become stable appears at the point that is 40 times the length of hydraulic diameter.eter.

• 대한기계학회논문집B
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• 제39권1호
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• pp.89-95
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• 2015

터보압축기의 서지는 압축기의 불안정 운전영역으로 주로 소음과 맥동을 유발하며 수회 지속될시 압축기 시스템 전반에 걸쳐 막대한 피해를 입힌다. 압축기의 안전한 운전을 위해서는 서지현상에 대한 특성파악과 제어전략 수립이 중요하다. 서지현상의 제어는 주로 압축가스의 통과유동량 증대, 필요한 헤드 저감, 압축기 회전수 감속, 가스의 바이패스를 통하여 이루어진다. 본 연구에서는 차량용 터보차저에 서지를 유발했을 때 각 운전 구간별 발생되는 압력변동 특성을 연구하고자 한다. 서지 특성 확인을 위한 파라미터는 압축기 입구 유량과 출구 유량, 관경, 회전수 등으로 선정하였다. 입구단과 출구단 유량을 조절하여 서지 압력 변동을 조사한 결과, 출구단 보다는 입구단 유량의 급격한 변화가 서지와 압축기 내구에 더 영향이 크다는 것을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제23권4호
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• pp.533-542
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• 1999

In this study the flow characteristics of developing turbulent pulsating flows in a square-sec-tional 180。 curved duct are investigated experimentally. The experimental study of air flow in a square-sectional curved duct is carried out to measure axial velocity distribution secondary flow velocity profiles and wall shear stress distributions by using a Laser Doppler Velocimetry system with the data acquisition and processing system of Rotating Machinery Resolver (RMR) and PHASE software at the entrance region of the duct which is divided into 7 sections from the inlet(${{\o}}=0_{\circ}$) to the outlet (${{\o}}=180_{\circ}$) in $30_{\circ}$ intervals. The results obtained from the study are summarized as follows: (1) The time-averaged critical Dean number of turbulent pulsating flow(De ta, cr) is greater than $75{\omega}+$ It is understood that the critical Dean number and the critical Reynolds number are related to the dimensionless angular frequency in a curved duct. (2) Axial velocity profiles of turbulent pulsating flows are of an annular type similar to those of turbulent stead flows. (3) Secondary flows of trubulent pulsating flows are strong and complex at the entrance region. As velocity amplitudes(A1) become larger secondary flows become stronger. (4) Wall shear stress distributions of turbulent pulsating flows in a square-sectional $180_{\circ}$ curved duct are exposed variously in the outer wall and are stabilized in the inner wall without regard to the phase angle.