• Journal of KSNVE
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• v.8 no.3
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• pp.477-484
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• 1998

An analytical procedure on the base of the substructure synthesis and assumed modes method is developed to investigate the flexibility effect of bladed disk assembly on vibrational modes of flexible rotor system. In modeling the system, Coriolis forces, gyroscopic moments, and centrifugal stiffening effects are taken into account. The coupled vibrations between the shaft and bladed disk are then extensively investigated through the numerical simulation of simplified models, with varying the shaft rotational speed and the prewist and stagger angles of the blade. It is found that the Coriolis and inertia forces and the inertia torque, which are induced by the one nodal diameter modes of the bladed disk and vary depending upon the stagger and prewist angles, lead to the coupled motions of the shaft and the bladed disk.

• Proceedings of the KIEE Conference
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• 2008.05a
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• pp.135-136
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• 2008

본 연구에서는 100GHz 이상의 높은 주파수에서 발진하는 초고주파 발생장치의 연구를 하였다. 전자파를 이용한 발진장치에서 대구경 후진파에 입사하는 전자빔의 크기와 상태를 좋게 하여 동작특성을 증진시키는 실험을 하여 그에 따른 변화 및 결과를 조사하였다. 출력의 증대와 방사할 때의 크기 및 그에 따른 주파수 교정, 그리고 마이크로파의 발진모드 특성을 분석하였다. 이는 주기의 크기에 따른 발진 주파수와의 관계를 분석하였으며 자기장의 변화 등 여러 가지 형태의 조건에 따른 결과를 나타내었다.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2010.03b
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• pp.39-39
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• 2010

낮은 에너지를 이용하여 상대론적 영역에서 동작하는 마이크로파 출력장치를 연구하였다 그에 따른 후진파 발진기는 대전력 마이크로파를 발생시키는 장치로서 연구하였으며 관내에 전자빔을 입사시킴으로서 발진이 일어나 출력을 발생 시킨다.

• The Science & Technology
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• v.31 no.4 s.347
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• pp.22-23
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• 1998

세계적인 광통신전문가인 백운출(광주과학기술원 정보통신공학과)교수는 지난19890년 세계최초로 장파장용 단일모드 광섬유로서 광분산이 일어나지 않는 광섬유를 설계했고 '86년에 초고속 광섬유 연출공법을 개발함으로써 광섬유를 실용화하는 쾌거를 이뤘으며 이 공적으로 미국 학술원 회원으로 추대되는 영광을 안았다. '91년 미국에서 이룬 모든 학문적 업적을 뒤로 한 채 귀국하여 광주과학기술원에서 후진 양성에 힘을 쏟고 있는 백교수는 21세기 우리나라가 정보통신을 리할 수 있도록 하는 마지막연구열을 불태우고 있다.

• Journal of the Society of Naval Architects of Korea
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• v.29 no.3
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• pp.90-101
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• 1992

Some practical methods have already been proposed for predicting the characteristics of ship manoeuvring motions at relatively high advance speed. However, these methods can hardly be applied to motions of ships in starting, stoppint, backing and slow steaming conditions, even though such extensive motions are of vital importance from a safety point of view particularly in harbour areas. The method presented here aims at predicting the characteristics of ship manoeuvring at low advance speed, which covers starting, stopping, backing and slow steaming conditions. The force mathematical models at large angles of incidence to the hull as well as under the tilde range of propeller operations are formulated. Simulations of various manoeuvres at low advance speed are carried out for two types of merchant ship, i.e. a LNGC and a VLCC. Comparisons between simulations and corresponding full-scale measurements or free-running model tests provide a first verification of the proposed mathematical models.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.10
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• pp.823-832
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• 2018

In general, the fidelity of the aircraft dynamic model is verified by comparison with the flight test results of the target aircraft. Therefore, the reference flight data for performance comparisons must be extracted. This process requires a lot of time and manpower to extract useful data from the vast quantity of flight test data containing various noise for comparing fidelity. In particular, processing of flight data is complex because rotorcraft have high non-linearity characteristics such as coupling and wake interference effect and perform various maneuvers such as hover and backward flight. This study defines flight data processing criteria for rotorcraft and provides procedures and methods for automated processing of static and dynamic flight data using data mining techniques. Finally, the methods presented are validated using flight data.