• 제목/요약/키워드: loads analysis

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중형항공기 주익 구조개발 선행연구를 위한 비행하중해석 (Flight Loads Analysis for Conceptual Study of the Regional Aircraft Wing Structure)

  • 신정우;강왕구;김성준;황인희
    • 한국항공운항학회지
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    • 제19권4호
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    • pp.67-73
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    • 2011
  • For loads analysis of airplane, applicable regulation should be determined. Then, loads conditions are prepared from the regulation. Modeling for aerodynamic, mass, and structure are performed. Panel method is usually adopted for aircraft loads analysis to obtain air loads. The ARGON which is a multidisciplinary fixed wing aircraft design software co-developed by the KARI and TsAGI are used for loads analysis. The ARGON can be utilized for flutter and stress analysis as well as for flight and ground loads analysis. In this paper, flight loads analysis for wing structural design of the regional aircraft at the conceptual design phase are performed with the ARGON. FAR 25 is used for the regulation for the load analysis. Shear force, bending moment and torsion diagrams for the wing and shear force and hinge moment for the aileron are presented.

Application of Equivalent Walking Loads for Efficient Analysis of Floor Vibration Induced by Walking

  • 김기철;김재열
    • 한국공간구조학회논문집
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    • 제4권4호
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    • pp.65-76
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    • 2004
  • Walking loads are usually considered as nodal loads in the finite element vibration analysis of structures subjected to walking loads. Since most of the walking loads act on elements not nodes, the walking loads applied on the elements should be converted to the equivalent nodal walking loads. This paper begins with measuring walking loads by using a force plate equipped with load cells and investigates the characteristics of the walking loads with various walking rates. It is found that the walking loads are more affected by walking rates than other parameters such as pedestrian weight, type of footwear, surface condition of floor etc. The measured walking loads are used as input loads for a finite element model of walking induced vibration. Finally, this paper proposes the equivalent nodal walking loads that are converted from the walking loads acting on elements based on finite element shape functions. And the proposed equivalent walking loads are proved to be applicable for efficient analysis of floor vibration induced by walking loads.

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4인승 선미익 경항공기 비행하중 해석

  • 신정우;김태욱;이상욱;심재열;황인희
    • 항공우주기술
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    • 제4권1호
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    • pp.1-8
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    • 2005
  • 미감항규정인 FAR과 이에 기반한 하중해석 절차를 설명하였다. 하중해석을 위해서는 규정과 하중조건을 준비하고, 공기력, 중량 및 구조 모델링을 수행해야 한다. 항공기 비행하중 해석시 공기력은 일반적으로 패널방법을 이용하여 산출하게 된다. 본 연구에서는 하중해석을 위해 In-house 프로그램인 ARGON을 사용하였다. ARGON은 KARI와 TsAGI가 공동 개발한 고정익 항공기 설계 프로그램으로서 비행하중, 지상하중, 플러터 및 응력해석을 지원한다. 본 논문에서는 ARGON을 이용하여 4인승 선미익 항공기 개발에 있어 필수적인 비행하중 해석을 수행하였고 그 결과를 제시하였다.

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ARGON을 이용한 스마트 무인기 비행하중해석 (Loads Analysis of Smart UAV Using ARGON)

  • 신정우;김성찬;황인희
    • 한국항공우주학회지
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    • 제33권7호
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    • pp.76-84
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    • 2005
  • 스마트 무인기 비행하중해석을 위해서는 규정과 하중조건을 준비하고, 공기력, 중량 및 구조 모델링을 수행해야 한다. 항공기 비행하중 해석시 공기력은 일반적으로 패널방법을 이용하여 산출하게 된다. 본 연구에서는 하중해석을 위해 In-house 프로그램인 ARGON을 사용하였다. ARGON은 KARI와 TsAGI가 공동 개발한 고정익 항공기 설계 프로그램으로서 비행하중, 지상하중, 플러터 및 응력해석을 지원한다. 본 논문에서는 FAR 23급 항공기인 스마트 무인기의 비행하중해석을 ARGON을 이용하여 수행하였고 그 결과를 제시하였다.

바닥판 진동해석을 위한 보행하중의 모형화 (Modeling of Walking Loads for Floor Vibration Analysis)

  • 김기철;최균호;이동근
    • 한국전산구조공학회논문집
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    • 제15권1호
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    • pp.173-188
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    • 2002
  • 보행하중을 받는 바닥판 구조물의 진동해석을 위해서 일반적으로 계측한 보행하중을 적용하거나 Bachmann의 보행하중식을 사용하게 된다. 다양한 매개변수의 영향을 받는 보행하중은 계측이 쉽지 않으며 Bachmann 보행하중식은 보행진동수가 2.OHz와 2.4Hz로 제한적이기 때문에 다양한 보행진동수에 따른 보행하중을 적용하기가 곤란하다. 따라서 보행하중을 받는 구조물의 진동해석을 위해서 보행하중의 매개변수 분석과 다양한 보행진동수에 적용이 가능한 보행하중의 모형화가 필요하다. 본 논문에서는 로드셀이 장착된 계측 플레이트를 이용하여 바닥판에 가해지는 보행하중을 직접 계측하고 매개변수를 분석하였다. 그리고 퓨리에 변환을 이용하여 계측한 보행하중을 다양한 진동수를 가지는 조화하중으로 분해하였다. 분해과정을 거쳐 얻은 조화하중의 계수들을 보행진동수에 대한 일정한 함수관계로 유도하여 보행하중을 모형화하였다. 본 논문에서 제안한 보행하중식을 이용하면 다양한 보행진동수에 따라 다르게 나타나는 보행하중을 구조물의 진동해석에 용이하게 적용할 수 있다.

스마트 무인기 비행하중 해석 (Flight Loads Analysis of Smart UAV)

  • 신정우;이상욱;김성준;김태욱;김성찬;황인희
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.513-518
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    • 2004
  • KARI(Korea Aerospace Research Institute) has developed smart unmaned aerial vehicle(UAV) since 2002. Smart UAV has tilt rotor configuration which can take off and land vertically. For designing and developing smart UAV, it is necessary to obtain design loads. ARGON which use the panel method is multidisciplinary aircraft design program developed and modified by KARI and TsAGI. Panel method is very useful to obtain aerodynamic loads, so it have been used widely for aircraft loads analysis. For flight loads analysis, we have to prepare regulations and load conditions, and then design aerodynamic panel model, mass model and structure model. In this paper, we introduce the flight loads analysis procedure briefly, and show the smart UAV loads analysis procedure and result using ARGON.

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보행하중을 받는 구조물의 효율적인 진동해석

  • 김기철
    • 한국지진공학회:학술대회논문집
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    • 한국지진공학회 2000년도 추계 학술발표회 논문집 Proceedings of EESK Conference-Fall 2000
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    • pp.159-166
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    • 2000
  • Structures with a long span have a higher possibility of experiencing excessive vibration induced by human activities such as walking, running, jumping and dancing. These excessive vibration give occupants annoyance. The general method for the vibration analysis of structures subjected to walking loads is to apply a series of nodal loads with assigned time delays at the nodes. But this method has a limit in representing the walking loads. In this study, the equivalent nodal loads are introduced for an effective analysis of floor vibration induced by walking loads. And, walking loads with difference walking rate are measured and applied to the analytical model for numerical analysis.

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요소 중심의 네트워크 접근법을 이용한 부정정 트러스 구조 해석 (Analysis of Indeterminate Truss Structures by Element-Focused Network Approach)

  • 한이철
    • 한국농공학회논문집
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    • 제58권3호
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    • pp.13-19
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    • 2016
  • Element-focused network analysis method for truss structure is proposed. The propagation process of loads from external loads to connected other elements is similar to that of connections between nodes in accordance with attachment rule in a network. Here nodes indicate elements in a truss structure and edges represent propagated loads. Therefore, the flows of loads in a truss structure can be calculated using the network analysis method, and consequently the structure can also be analyzed. As a first step to analyze a truss structure as a network, we propose a local load transfer rule in accordance with the topology of elements, and then analyze the loads of the truss elements. Application of this method reveal that the internal loads and reactions caused by external loads can be accurately estimated. Consequently, truss structures can be considered as networks and network analysis method can be applied to further complex truss structures.

보행하중을 받는 건축물 바닥판의 진동해석 (Vibration Analysis of Building Floor Subjected to Walking Loads)

  • 김기철;이동근
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2001년도 봄 학술발표회 논문집
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    • pp.414-421
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    • 2001
  • Recently, the damping effect of building structures are greatly reduced because the use of non-structures members as like curtain wall are decreased and large open space are in need for the service of buildings. Assembly and office buildings with a lower natural frequency have a higher possibility of experiencing excessive vibration induced by human activities as like jumping, running and walking. These excessive vibration make the occupants uncomfortable and the serviceability deterioration. The common method of application of walking loads for the vibration analysis of structures subjected to walking loads is to inflict a series unit walking load and a periodic function at a node. But this method could not consider the moving effect of walking. In this study, natural frequency and damping ratio of plate structure are evaluated by heel drop tests. And new application of equivalent walking loads are introduced for vibration analysis of real slab system subjected to walking loads. The response obtained from the numerical analysis are compared well to the results measured by experimental tests. It is possible to efficiently analyze the vibration of floor which is subjected to walking loads by applying equivalent walking loads.

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변위에 기초한 동하중에서 변환된 등가정하중하에서의 구조최적설계 (Structural Optimization under Equivalent Static Loads Transformed from Dynamic Loads Based on Displacement)

  • 강병수;최우석;박경진
    • 대한기계학회논문집A
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    • 제24권8호
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    • pp.1949-1957
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    • 2000
  • All the loads in the real world act dynamically on structures. Since dynamic loads are extremely difficult to handle in analysis and design, static loads are utilized with dynamic factors. The dyna mic factors are generally determined based on experiences. Therefore, the static loads can cause problems in precise analysis and design. An analytical method based on modal analysis has been proposed for the transformation of dynamic loads into equivalent static load sets. Equivalent static load sets are calculated to generate an identical displacement field in a structure with that from dynamic loads at a certain time. The process is derived and evaluated mathematically. The method is verified through numerical tests. Various characteristics are identified to match the dynamic and the static behaviors. For example, the opposite direction of a dynamic load should be considered due to the vibration response. A dynamic bad is transformed to multiple equivalent static loads according to the number of the critical times. The places of the equivalent static load can be different from those of the dynamic load. An optimization method is defined to use the equivalent static loads. The developed optimization process has the same effect as the dynamic optimization which uses the dynamic loads directly. Standard examples are solved and the results are discussed