• 한국국방경영분석학회지
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• 제34권2호
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• pp.1-26
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• 2008

본 연구에서는 현재 우리나라 육군이 사용하고 있는 보병화기와 포병화기(155M)의 기본 휴대량(B/L : Basic Load) 개념 정립 및 산정방법을 고찰하여 문제점을 도출하고 시뮬레이션 기법(ARENA Model)을 통해 최적의 B/L을 재산정하여 제시하였다. 본 논문을 통한 기대효과는 군수지원의 물동량 감소로 실질적인 전투 준비 태세 강화와 국방예산 절감이 예상되며, 효율적인 B/L운영 보장으로 전투 효율성을 증대시킴은 물론 궁극적으로 전장 승리를 보장하는데 기여할 것이다.

• 한국안전학회지
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• 제29권2호
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• pp.53-61
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• 2014

This study evaluated wind loads considering a local basic wind velocity and construction periods to define the level of applied wind loads for system supports. Structural responses of system supports were examined and compared to those of system supports with the level of wind loads following various standards and specifications for permanent and temporary structures. And, the maximum combined stress ratios were estimated to evaluate the structural safety of a considered system support. From results, it was found that the wind load level should be applied in accordance with construction periods when estimating the safety of system supports. Looking into the response by change of the basic wind velocity according to local regions, it is no need to consider wind loads in regions with the basic wind velocity of 30 m/s. However, it was analyzed that wind loads should be considered in the regions with the basic wind velocity of 40 m/s or above. In addition, wind loads should be considered in designing system supports located at the region with the basic wind velocity of 35 m/s starting from construction period of 1.5 years. The standard specification for temporary work was analyzed as an incorrect standard in evaluating wind loads, since it underestimated the response of system supports in accordance with the local basic wind velocity and construction periods.

• 대한교통학회지
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• 제17권2호
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• pp.69-79
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• 1999

본 연구에서는 고속도로의 기본구간과 비교해 볼 때, 고속도로 합류부에서의 운전자의 각성정도의 변화를 생리적 신호 중 후두엽부(Occipital Lobe)의 뇌파 중 $\beta$파를 측정하여 정량화하여 살펴보았다. 고속도로 기본구간 3지점과 합류부 구간 3지점에서 실험차량을 이용하여 남자 8명, 여자 2명, 총 10명의 피실험자를 대상으로 실험한 결과 고속도로 운전자는 합류부 구간(램프주행구간, 가속차로시점에서 합류직전 구간, 합류부 영향이 남아 있는 주행구간)에서 운전시 기본 주행구간에 비하여 가속차로 시점에서 합류 직전구간에서 2.21배로 가장 큰 각성정도를 보였다. 또한 고속도로 운전자는 합류를 완료한 후에 4초간 합류과정으로 인한 영향이 남아 있는 것으로 분석되었다. 특히 운전자들은 고어지점으로부터 80m구간이내에서 합류하는 것이 충분한 가속주행을 한 것보다 더 각성 정도를 보였다.

• 대한조선학회 특별논문집
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• 대한조선학회 2005년도 특별논문집
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• pp.31-37
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• 2005

An attempt to improve the speed performance through the minimizing in wave resistance has been done by an application of gooseneck and no bulb type to bulbous bow for the DSME 78,500 Class LPG Carrier on the basis of the CFD calculation and comparatives model tests. The hydrodynamic characteristics according to the variation of the shape of Cp-curve, design load water line, frame line and bulbous bow that have an important effect on the wave resistance has been evaluated/calculated by ship-flow code. A wide variety in hull variation have been tried to have a good hull form with three types of fore-body hull forms mainly classified by the shape of bulbous bow. The speed performances for the three final hull forms with different bulbous bows have been evaluated through the model tests.

• 한국해양공학회지
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• 제29권3호
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• pp.207-216
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• 2015

Amanifold is one of the essential subsea oil and gas production components to simplify the subsea production layout. It collects the production fluid from a couple of wellheads, transfers it to onshore or offshore storage platforms, and even accommodates water and gas injection flowlines. This paper presents the basic design procedure for a manifold frame structure with novel structural verification using in-house unity check codes. Loads and load cases for the design of an SIL 3 class-manifold are established from a survey of relevant industrial codes. The basic design of the manifold frame is developed based on simple load considerations such as the self weights of the manifold frame and pipeline system. In-house software with Eurocode 3 embedded, called INHA-SOLVER, makes it possible to carry out code checks on the yield and buckling unities. This paper finally proves that the new design of the manifold frame structure is effective to resist a permanent and environment load, and the in-house code is also adaptively combined with the commercial finite element code Nastran.

• Structural Engineering and Mechanics
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• 제70권2호
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• pp.245-255
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• 2019

In present research, we have considered transversely isotropic magneto thermoelastic solid with two temperature and without energy dissipation due to inclined load. The mathematical model has been formulated using Lord-Shulman theory. The Laplace and Fourier transform techniques have been used to find the solution to the problem. The displacement components, stress components and conductive temperature distribution with the horizontal distance are computed in the transformed domain and further calculated in the physical domain using numerical inversion techniques. The effect of rotation and angle of inclination of inclined load is depicted graphically on the resulting quantities.

• Structural Engineering and Mechanics
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• 제81권5호
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• pp.529-537
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• 2022

The present research is to study the effect of inclined load in a two-dimensional homogeneous orthotropic magneto-thermoelastic solid without energy dissipation with fractional order heat transfer in generalized thermoelasticity with two-temperature. We obtain the solution to the problem with the help of Laplace and Fourier transformations. The field equations of displacement components, stress components and conductive temperature are computed in transformed domain. Further the results are computed in physical domain by using numerical inversion method. The effect of fractional order parameter and inclined load has been depicted on the resulting quantities with the help of graphs.

• 항공우주기술
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• 제1권1호
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• pp.8-27
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• 2002

본 연구에서는 현재 개발중에 있는 복합재료 선미익 항공기의 날개에 작용하는 하중해석을 수행하였다. 중량, 공력계수, 구조설계속도, 하중 등을 계산하기 위해 사용된 Tool은 Excel에서 운용되는 Visual Basic 프로그램으로 계산에 많은 도움을 주었다. 하중해석에 기본적으로 요구되는 항공기의 형상치수, 부품의 종류 및 중량 그리고 좌표계 등은 Catia 모델링, 실제측정 또는 재료밀도 값 등을 이용해 구하였으며, 이들 자료를 통하여 항공기의 중량, 무게중심, 관성모멘트, 구조설계속도, 날개의 하중분포, 힘과 모멘트 등을 계산하였다. 또한 항공기의 날개 및 동체의 임계하중 조건을 선정하는데 필수적인 항공기의 V-n 선도를 도시하였으며, 이 V-n 선도는 항공기의 최대중량 2,573 파운드 및 해면고도조건에서 설계속도 $V_A$, $V_C$, $V_D$ 및 하중계수 +3.8G, -1.52G에 대한 비행범위를 제시하고 있다. 앞으로는 V-n 선도로부터 선정된 임계하중을 이용하여 해석된 동체 및 날개에 대한 하중을 제시하고자 한다.

• 한국건축시공학회:학술대회논문집
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• 한국건축시공학회 2013년도 추계 학술논문 발표대회
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• pp.188-189
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• 2013

The purpose of this research is to comprehend experimentally the characteristic of human dynamic load and provide the result as basic data to suggest a valid impact-resistance evaluation method. Human motions exerting dynamic load are classified to 3 types. Selecting 3 ranks of motion strength, 3 ranks of load plane stiffness (A:20kN/cm, B:4.7kN/cm, C:2.2kN/cm), and 30 male grownup inspectors in their twenties, load was measured when they applied force on load plane. Result of this research is as follows: (1) Human dynamic load has different nature from object collision in the highest load ratio depending on the load plane stiffness and action time (2) The highest load ratio for each motion was 10.06 for kicking, 4.44 for hitting with shoulder, and 5.58 for fist blow.

• 환경위생공학
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• 제20권3호
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• pp.51-56
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• 2005

Allocation of water pollution load from loading capacity can be much essential, controversial, and its standards can be applied case-by-case to the various situations. Allocation methods to point sources are generally 'Equal effluent concentration', 'Equal percent Treatment', Loading capacity at planning stage consists of basic pollution load, development pollution load, reserved pollution load and margin of safety. But at the implementing stage loading capacity can be consisted of allocatable load and margin of safety to give more flexibility in the total water pollution load management plan. In that case, we can re-adjust and altogether use the pollution load of point sources of series and non-point sources at the implementing stage.