• 항공우주시스템공학회지
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• 제1권1호
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• pp.36-44
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• 2007

This study was performed on preliminary structural design of a small scale WIG craft which has been developed as a next generation high speed maritime transportation system in Korea. A composite structure design using the foam-sandwich for main wing and tail fins and the honeycomb sandwich and skin-stringer-ring frame for fuselage was applied for weight reduction as well as structural stability. A commercial FEM code, NASTRAN for was utilized to confirm the structural safety for the reiterate design modifications to meet design requirements including the target weight. Each main wing was jointed with the fuselage by eight high strength insert bolts for easy assembling and disassembling as well as for assuring the required 20 years service life. For control surface structural design, the channel type spar, the foam sandwich skin and the lug joint were adopted.

• International Journal of Aerospace System Engineering
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• 제7권1호
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• pp.7-15
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• 2020

In this paper the crack growth, modeling, and simulation of the stiffened and un-stiffened cracked panels presented using commercially available finite element software packages. Computation of stresses and convergence of stress intensity factor for single edge notch (SEN) specimens carried out using the finite element method (FEM) and extended finite element method (XFEM) and compared with an analytical solution. XFEM techniques like cohesive segment method and LEFM using virtual crack closure technique (VCCT), used for crack growth analysis and presented results for un-stiffened and stiffened panels considering various crack domain. The non-linear analysis considering both geometric and material non-linearity on stiffened panels with various stringers like a blade, L, inverted T and Z sections the results were presented. Arrived at the optimum stringer section type for the considered panel under axial loading from the numerical analysis.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.631-636
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• 2008

The cylindrical shells are mainly used in the nuclear energy structure, pressure vessel, boiler and so on. When designing of shell structures, predicting the structure change under variety boundary conditions are necessary for estimating the safety. Design variables for the design engineer include multiple material systems and boundary conditions, in addition to overall structural design parameters. Since the vibration of stiffened cylindrical shell is an important consideration for structures design, the reliable prediction method and design methodology should be required. In this study, the optimum design of stiffened cylindrical shell for maximum natural frequency was studied by analytic and numerical method.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2001년도 추계학술대회 논문집 Vol.14 No.1
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• pp.189-192
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• 2001

Recently, STI process is getting attention as a necessary technology for making high density of semiconductor by devices isolation method. However, it does have various problems caused by CMP nprocess, such as torn oxide defects, nitride residues on oxide, damages of si active region, contaminations due to post-CMP cleaning, difficulty of accurate end point detection in CMP process, etc. In this work, the various defects induced by CMP process was introduced and the above mentioned problems of CMP process was examined in detail. Finally, the guideline of future CMP process was presented to reduce the effects of these defects.

• 한국정밀공학회지
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• 제20권2호
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• pp.136-145
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• 2003

The integrity of stiffened panels with stringers in airplane structure is generally enhanced by investigating the fatigue crack propagation behavior in detail and providing the technical methodology to deal with the propagating crack. This paper attempts to clarify the effect of load-ratio on the fatigue crack propagation rate and the fatigue life for the thin aluminum 2024-T3. Both the variable and the constant fatigue loading conditions are considered for the fatigue crack propagation behavior in stiffened panels with stringers.

• Journal of Ship and Ocean Technology
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• 제5권4호
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• pp.19-28
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• 2001

A comparative study of the new flexible double hull structure is presented as a collision energy absorbing system, which is constructed with mixed stringers comprising slant and straight stringers for the double hull tanker, The dimension and disposition of this mixed stringers are selected to give the maximum absorbing energy. From the viewpoint of collision energy absorbing efficiency, this structural system is compared with three other types of the double hull constructions with trapezoidal stiffener, stringer type and standard type of VLCC, 310K DWT, Based on the constant hull weight, the proposed double hull structure with mixed stringers shows a improved crashworthiness as the results.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.157-160
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• 2000

In author's previous paper, a finite element algorithm was presented to calculate the buckling and crippling stresses of composite laminated stringers. In this study, for the validation of the finite element analysis, Z-section composite stringers of different lengths and flange-widths were tested in axial compression. The stacking sequence of graphite/epoxy is [$\pm$45/0/90]s. Strain gages were attached to each specimen to get the strain response. Deflection and end-shortening were obtained by a displacement transducer. The buckling and crippling loads are determined from the strain response, load vs. end-shortening curves, and load vs. out-of-plane deflection curves. Comparison between finite element and experimental results shows good agreement in the buckling, local buckling, and crippling stresses.

• Steel and Composite Structures
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• 제14권5호
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• pp.511-521
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• 2013

In this study we have considered the governing nonlinear equation of an eccentrically reinforced cylindrical shell. A new analytical method called He's Variational Approach (VA) is used to obtain the natural frequency of the nonlinear equation. This analytical representation gives excellent approximations to the numerical solution for the whole range of the oscillation amplitude, reducing the respective error of angular frequency in comparison with the variation approach method. It has been proved that the variational approach is very effective, convenient and does not require any linearization or small perturbation. Additionally it has been demonstrated that the variational approach is adequately accurate to nonlinear problems in physics and engineering.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2001년도 추계학술대회 논문집
• /
• pp.189-192
• /
• 2001

Recently, STI process is getting attention as a necessary technology for making high density of semiconductor by devices isolation method. However, it does have various problems caused by CMP process, such as torn oxide defects, nitride residues on oxide, damages of si active region, contaminations due to post-CMP cleaning, difficulty of accurate end point detection in CMP process, etc. In this work, the various defects induced by CMP process was introduced and the above mentioned Problems of CMP process was examined in detail. Finally, the guideline of future CMP process was presented to reduce the effects of these defects.

• 한국강구조학회 논문집
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• 제26권6호
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• pp.511-522
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• 2014

본 연구에서는 주거용 및 사무용 계단시공의 작업공정의 단순화 및 시공품질 향상을 목적으로 개발된 혁신적인 계단 시스템인 슬라이딩스텝 철골계단의 진동 및 구조성능 평가를 수행하였다. 슬라이딩스텝 철골계단은 각형 강재 스트링거와 시공오차를 흡수할 수 있도록 설계된 스트링거 연결재 및 계단벽체 시공이 용이하도록 벽체 반대방향으로 이동이 가능한 슬라이딩 스텝으로 구성되어 있다. 하지만 철골계단의 경우 철골 접합부의 구조적 안전성 확보와 더불어, 비교적 경량에 저감쇠인 철골재 사용으로 인한 낮은 진동성능이 발현될 수 있기 때문에 진동성능에 대한 확보를 파악하는 것이 필수적으로 요구된다. 이에 본 연구에서는 진동성능 및 구조적 안전성 확보여부를 파악하기 위해 실물대 목업실험을 실시하였다. 진동성능 및 중량으로 인한 경제성 등을 종합적으로 판단하기 위해 콘크리트를 채운 스트링거와 콘크리트를 채우지 않은 스트링거를 교체해가며 각 경우에 대한 주거용 및 사무용 계단의 진동성능을 평가하였다. 또한 각 용도별로 한 개의 계단을 선정한 후, 재하실험을 통해 철골 접합부의 구조적 안전성과 스트링거 중앙부의 잔류 처짐 및 사용성 검토를 수행하였다. 실물대목업실험 결과 접합부 시스템의 경우 사용하중의 160%인 극한하중에 대해서도 탄성상태를 유지하며 재하실험 후에도 어떠한 균열이나 이상이 발견되지 않는 등 충분한 강성과 강도를 확보하고 있음을 확인하였다. 또한 스트링거 중앙부 처짐은 주거용/사무용 계단 모두 역시 동일한 하중조건 하에서 사용성에 문제가 없을 정도의 미미한 수준의 최대처짐과 잔류처짐이 발생하였으며, 최대하중이 가해질 때까지 스트링거가 탄성상태를 유지하는 등 설계하중을 지지할 수 있는 충분한 내력을 보유한 것으로 평가되었다. 진동성능 검토 결과 총 일곱 개의 스트링거 타입 중 다섯 개의 타입이 북미기준와 유럽기준에서 제시하는 기준의 허용치를 만족함을 확인하였다.