• International Journal of Aerospace System Engineering
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• 제2권2호
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• pp.79-82
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• 2015

The handicap for investigating the aero-optical effect focuses on the accurate prediction on the index refraction fluctuation or density fluctuation. In recent years, with the development of CFD techniques and optical experimental techniques, the comprehension have developed on the aero-optical transmitting effect in many kinds of complex flow. This study mainly introduces the optical aberration in compressible mixing layer. And then the debates about the mechanism of aero-optical effects and assessment of image blur also present.

• 한국광학회지
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• 제8권1호
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• pp.73-79
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• 1997

랜드/그루브 기록 광디스크에서 랜드와 그루브의 영향, 각종 수차 그리고 수광계의 변화가 포커스에러신호에 미치는 영향을 나이프엣지법과 비점수차법으로 구분하여 시뮬레이션을 통해 분석하였다. 그루브의 영향에 의해 포커스에러신호에서 Aero Cross 점이 Shift되는데, 이는 디스크 반사 회절빔의 파면이 Defocus 성분을 포함하고 있기 때문이라는 것을 밝혔다. 또한 회절빔의 각 차수별로 포커스에러신호를 분석함으로써 빔점수차 방식에서 랜드와 그루브의 영향으로 에러신호의 감도가 감소함을 보았다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 춘계학술대회논문집
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• pp.677-683
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• 2002

The analytical and experimental studies on aerodynamic flutter instability of rotating disks in information storage devices are investigated. The theoretical analysis uses a fluid-structure model where the aerodynamic force on the rotating disk is represented in terms of lift and damping forces. Based on the analytical approach, it is shown that the backward natural frequency of the disk is equal to that of the case without aerodynamic effect at the flutter onset speed. In post-flutter regions, the natural frequencies are larger than those in vacuum conditions without aerodynamic effect. The analytical predictions on the natural frequencies of rotating disks with/without aerodynamic effect are experimentally verified using a vacuum chamber and ASMO optical disks.