• 한국광학회지
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• 제7권1호
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• pp.37-43
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• 1996

횡자장하에서 Zeeman 안정화된 He-Ne 레이저를 광원으로 한 두 종류의 공기굴절율 측정용 간섭계를 설계.제작하였다. 제작된 간섭계는 레이저 광속이 진공조와 기체조를 2번 혹은 4변 지나도록 설계하여 분해능을 향상시켰으며 그 경로가 진공조를 중심으로 대칭적으로 지나도록 설계하여 열적인 변형 및 기계적인 진동에 강한 특성을 갖도록 하였다. 진공조와 기체조 사이의 광로차를 위상각 검출 방식의 heterodyne 간섭계로 측정하므로써 homodyne 간섭계에서 발생되는 간섭무늬 해석 오차를 최소화시켜 공기굴절율 측정의 정확도를 향상시켰다. 제작된 두 굴절율계를 이용하여 여러 조건에서 공기굴절율을 측정한 결과 평균값에서의 상호 편차는 $2\times10^{-8}$ 이하였으며 Edlen공식을 이용한 굴절율계와의 편차는 $1\times10^{-7}$ 이하였다.

• 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.