• Korean Architects
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• no.4 s.288
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• pp.18-51
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• 1993

• Journal of Aerospace System Engineering
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• v.18 no.1
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• pp.21-28
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• 2024

In this paper, two prediction models based on deep neural network that could predict cross-sectional stiffness of a rotor blade were proposed. Herein, we employed structural and material information of cross-section. In the case of a prediction model that used material properties as the input of the network, it was designed to predict the cross-sectional stiffness by considering elastic modulus of each cross-sectional member. In the case of the prediction model that used structural information as a network input, it was designed to predict the cross-sectional stiffness by considering the location and thickness of cross-sectional members as network input. Both prediction models based on a deep neural network were realized using data obtained by cross-sectional analysis with KSAC2D (Konkuk section analysis code - two-dimensional).

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.354-359
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• 1995

회전익의 소재로 복합재료를 선택하게 됨에 따라 헬리콥터의 유지, 보수 및 성능에서 유리하게 되었지만 허브 형태의 간소화로 인하여 해석상의 어려움은 확대 되었다고 할 수 있을 것이다. 따라서 회전익의 단면특성은 더욱 중요한 의미를 갖게 되었다. 회전익의 단면특성을 결정하기 위해서 우선적으로 각 방향운동의 연성항을 소거하는 것이 계산상 유리하고 따라서 관성주축방향을 결정하는 것이 중요하다. 그러나 회전익의 익형이 대칭형이 아니고 복합한 재료로 구성되어 있을 뿐 아니라 효율의 극대화를 위하여 축방향을 따라 비틀림을 부여하고 있기 때문에 관성주축의 방향을 결정하는데 많은 어려움이 존재한다. 따라서 본 연구에서는 실제 회전익을 그 연구 대상으로 회전익 단면의 등가강성행렬을 추출하고 외팔보의 공학이론과 회전행렬을 이용하는 방법으로 관성주축방향을 결정하는 방법을 제시하였다. 해석방법의 타당성을 확보하기 위하여 엄밀해를 알고 있는 간단해 단면을 갖는 외팔보를 이용하여 검증하였다. 이러한 방법은 관성주축방향을 결정하는 새로운 프로그램의 개발이라는 부담을 최소화 하였을 뿐 아니라, 해석방법 자체가 가지는 간편성으로 인하여 많은 시간과 노력을 줄일수 있을 것으로 기대된다.

• Proceedings of the Korean Vacuum Society Conference
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• 1996.06a
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• pp.100-101
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• 1996

• Proceedings of the Materials Research Society of Korea Conference
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• 1995.11a
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• pp.43-43
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• 1995

• Magazine of the Korea Concrete Institute
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• v.9 no.6
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• pp.207-216
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• 1997

본연구는 축방향 변형 구속이 고강도 콘크리트 휨부재의 휨 전단거동에 미치는 영향을 조사하기 위한 것으로, 수화열과 건조수축에 기인하는 축방향 변형과 재하에 의한 축방향 변형을 구속한 부재 및 무구속 부재에 대하여 휨파괴와 전단파괴 실험을 실시하였다. 타설 직후부터 축변형을 구속한 실험체의 재하시 강성은 재하전의 구속으로 발생한 관통균열의 영향을 받아 무구속 실험체의 강성보다 낮지만, 재하시의 축변형 구속에 따른 압축구속력의 상승으로 인하여 강성의 크기는 역전되었다 축변형이 완전히 구속된 휨부재의 휨강도는 무구속 부재보다 20%이상 상승하지만 변형능력은 감소하는 것으로 나타났으며, 재하전의 축변형 구속에 의한 관통균열(균열폭 0.1mm 미만)은 부재의 전단내력 및 전단균열 진전 형상에 영향을 미치지 않았다.

• Geotechnical Engineering
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• v.7 no.4
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• pp.15-24
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• 1991

This paper reports the application study of the concrete bedding reinforcement under a buried conduit with flexible joints subjected to differential settlement via a finite elemen modeling. The reinforcement of concrete bedding helps to minimize the differential settlement between the adjoining conduit segments. Three different field conditions have been considered. The settlement pattern and deformation slope have been evaluated for each boundary condition. The analysis results are compared for both non-reinforced and reinforced cases to measure the effectiveness of concrete bedding reinforcement for restraining deformation of a conduit with flexible joints.

• Journal of Aerospace System Engineering
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• v.13 no.6
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• pp.52-59
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• 2019

The rotor blade is a key component that generates the lift, thrust, and control forces required for helicopter flight by the torque transmitted through the hub and the blade pitch angle control, and should be designed to factor vibration characteristics so that there is no risk of resonance with structural safety. In this study, the structural design of the main rotor blade for MPUH(Multi-Purpose Unmanned Helicopter) was conducted and the sectional stiffness measurement of the fabricated blade was performed. The evaluation of the vibration characteristics of the main rotor system was then conducted factoring the measured stiffness distribution. The interior of the rotor blade comprised of the skin, spar, and torsion box, and carbon and glass fiber composites were applied. The Ksec2D program was applied to predict the stiffness of blade, and the results were compared to the measured data. CAMRADII, a comprehensive rotorcraft analysis program, was applied to investigate the natural frequency trends and resonance risks due to the rotor rotation.

• Journal of the Korea institute for structural maintenance and inspection
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• v.8 no.4
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• pp.115-122
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• 2004

The objective of the present study is to understand the strengthening effects of reinforced concrete beam applied the reinforced plates, expended metal and carbon fiber grid with the ceramic metal. In the present study, the bending tests are performed to understand the increasing effects of stiffness and ductility for the strengthening RC beam. Also, the important purpose of the structural tests is to understand the adhesion performance of the ceramic metal. It is expected the present experimental observations as a valuable source in suggestion improved the strengthening method more than this method by analysis of the failure mode for the specimens.

• Journal of the Korean Society for Precision Engineering
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• v.22 no.9 s.174
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• pp.162-172
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• 2005

The objective of this research works is to investigate into characteristics of bending stiffness and failure for the ISB ultra-lightweight panel with internally structured material. The expanded metal with a crimped pyramid shape and woven metal are employed as an internally structured material. Through three-points bending test, the force-displacement curve and failure shape are obtained to examine the deformation pattern, characteristic data, such as maximum load, displacement at maximum load, etc, and failure pattern of the ISB panel. In addition, the influence of design parameters fur ISB panel on the specific stiffness, the specific stiffness per unit width, failure mode and failure map has been found. Finally, it has been shown that ISB containing expand metal with the crimped pyramidal shape is prefer to that containing woven metal from the view point of optimal design for ISB panel.