• 제목/요약/키워드: body-space

검색결과 1,640건 처리시간 0.023초

THE ATTITUDE STABILITY ANALYSIS OF A RIGID BODY WITH MULTI-ELASTIC APPENDAGES AND MULTI-LIQUID-FILLED CAVITIES USING THE CHETAEV METHOD

  • Kuang, Jin-Lu;Kim, Byung-Jin;Lee, Hyun-Woo;Sung, Dan-Keun
    • Journal of Astronomy and Space Sciences
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    • 제15권1호
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    • pp.209-220
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    • 1998
  • The stability problem of steady motion of a rigid body with multi-elastic appendages and multi-liquid-filled cavities, in the presence of no external forces or torque, is considered in this paper. The flexible appendages are modeled as the clamped -free-free-free rectangular plates, or/and as the discrete mass- spring sub-system. The motion of liquid in every single ellipsoidal cavity is modeled as the uniform vortex motion with a finite number of degrees of freedom. Assuming that stationary holonomic constraints imposed on the body allow its rotation about a spatially fixed axis, the equation of motion for such a systematic configuration can be very complex. It consists of a set of ordinary differential equations for the motion of the rigid body, the uniform rotation of the contained liquids, the motion of discrete elastic parts, and a set of partial differential equations for the elastic appendages supplemented by appropriate initial and boundary conditions. In addition, for such a hybrid system, under suitable assumptions, their equations of motion have four types of first integrals, i.e., energy and area, Helmholtz' constancy of liquid - vortexes, and the constant of the Poisson equation of motion. Chetaev's effective method for constructing Liapunov functions in the form of a set of first integrals of the equations of the perturbed motion is employed to investigate the sufficient stability conditions of steady motions of the complete system in the sense of Liapunov, i.e., with respect to the variables determining the motion of the solid body and to some quantities which define integrally the motion of flexible appendages. These sufficient conditions take into account the vortexes of the contained liquids, the vibration of the flexible components, and coupling among the liquid-elasticity solid.

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근접쌍성 V651 Cas의 공전주기 변화의 재논의 (REDISCUSSION OF PER100 CHANGE OF THE CLOSE BINARY V65l CASSIOPEIAE)

  • 김천휘;이재우;이충욱;이동주;강영운
    • Journal of Astronomy and Space Sciences
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    • 제19권1호
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    • pp.47-56
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    • 2002
  • 2000년 11월 21일부터 23일가지 3일간 식쌍성 V65l Cas의 극심시각 관측을 수행하였다. 이 관측으로부터 총7개의 새로운 극심시각을 얻었다. 이 관측치를 포함한 V651 Cas의 광전관측 및 CCD 극심시각을 재분석하여, 김천휘와 이재우(2000)가 제안한 제3 천체에 의한 광시간 궤도를 확인하였고, 개선하였다. 최종적으로 구한 광시간 궤도의 주기, 반-진폭, 그리고 이심율은 각각 $6.^{y}3,\;0.^{d}0013$, 그리고 0.78이다. 제3 천체의 궤도경사각이 $30^{\circ}$보다 클 경우, 제3 천체의 질량은 $0.09M_{\odot}\;{\leq}\;M_3\;{\leq}\;0.20M_{\odot}$의 범위에 있다. V65l Cas 계에 상정된 제3 천체가 진실로 존재하고, 주계열성이라면, 그 제3 천체는 주계열 끝에 위치한다.

CFD를 이용한 천음속 날개-동체 형상 해석 (Numerical Simulation for Transonic Wing-Body Configuration using CFD)

  • 김영화;강은지;안효근
    • 한국항공우주학회지
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    • 제45권3호
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    • pp.233-240
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    • 2017
  • 본 연구에서는 전산유체역학의 특징에 대한 이해를 위해 천음속 날개-동체 주위의 유동장을 In-house 전산유체 코드로 해석하여 시험 결과와 비교하였다. 날개는 RAE 101 익형 단면을 가진 RAE Wing 'A'이며 동체는 축대칭 형상이다. In-house 코드는 비정렬 격자 기반의 압축성 Euler/Navier-Stokes 해석 코드이다. 격자에 대한 의존도, 난류 모형, 공간차분 기법, 점성/비점성의 영향을 시험 결과와 비교하여 살펴보았다. 난류 모형은 $k-{\omega}$ 모형, Spalart-Allmaras 모형, $k-{\omega}$ SST을 적용하였고, 공간차분 기법은 Jameson의 인공 점성를 도입한 중앙 차분 기법과 Roe의 풍상 차분 기법을 적용하였다. 대체적으로 시험 결과를 잘 예측하였으나, 압력분포 및 충격파의 위치가 난류 모형 및 공간 차분 기법에 따라 조금씩 다르게 예측되었으며, 정확한 충격파 위치를 예측하기 위해서는 난류 점성 효과가 고려되어야 함을 알 수 있다.

원형 제한 3체 문제의 불변위상공간을 이용한 행성간 궤적설계 기초 연구 (Preliminary Study on Interplanetary Trajectory Design using Invariant Manifolds of the Circular Restricted Three Body Problem)

  • 정옥철;안상일;정대원;김은규;방효충
    • 한국항공우주학회지
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    • 제43권8호
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    • pp.692-698
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    • 2015
  • 본 논문에서는 원형 제한 3체 문제의 불변위상공간을 이용하여 지구-달 또는 행성간의 궤적을 설계하고 해석하는 기법을 소개한다. 2체 문제를 조합하는 고전적인 방식 대신에 원형 제한 3체 문제에 대한 운동방정식, 궤적의 동적 특성, 평형점 주변의 리아프누프 궤도와 불변위상공간의 특성을 기술한다. 원형 제한 3체 문제의 불변위상공간을 이용했을 때, 지구-달 시스템의 궤적설계 방식과 태양-목성 시스템의 경계면에서의 초기조건에 따른 궤적 특성을 수치 시뮬레이션을 통해 확인한다. 본 논문에서 제안한 원형 제한 3체 문제의 불변위상공간을 이용한 궤적설계 기법은 저추력 또는 저에너지를 이용한 달탐사 또는 행성탐사 임무 등에 활용 가능할 것이다.

신체적합성을 고려한 제깅스(Jeggings) 패턴 개발 -20~24세 여성을 중심으로- (Development of Jeggings Pattern Considering Body Fit -Focus on 20-24 Year Old Females-)

  • 이규선;최정욱
    • 한국의류학회지
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    • 제38권5호
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    • pp.675-689
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    • 2014
  • This study developed an ideal jeggings pattern with an improved body fit for 20-24 year old females. The results of the study are as follows. First, samples for wearing test were made using jegging patterns from three manufacturers; subsequently, one pattern with a relatively outstanding body fit was selected from the first test. The selected pattern suggested a tight knee, belly, and crotch, high front waist line, and low back waist line. The side lines were also lean to the front; consequently, the front hip width was extended for 0.5cm for more space around the belly and the extended front knee part for 0.2cm to increase moving suitability to fix the leaning side lines. A 1cm front waist line was extended for 0.5cm to fix it lower; in addition, the back waist line 3.0cm was extended for 0.5cm to heighten it. The crotch width was also extended for 0.5cm to add more space. The second wearing test for the fixed forms were evaluated for their outstanding features in appearance as well as moving functions that were proposed as final jeggings forms. The results of the study suggested a jeggings pattern with a better body fit using manufacturer patterns that can be used as basic data for pant patterns with better fitting using various stretch fabrics.

20대 여성의 Tight-fit원형설계에 관한 연구 (A Study of Tight-fit Bodice Pattern for 20's Women)

  • 정복희;나미향
    • 대한가정학회지
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    • 제39권8호
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    • pp.137-154
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    • 2001
  • This study was made to draft the tight fitting bodice pattern which horizontal and perpendicular stands are to be lightly set, with the consideration of characteristics of body shape in design of clothes. Measurement of body was conducted on 53 women in twenties, and observation was made on surface development pattern by adhesive tape addition method and gypsum method on three standard objects. In the study, bodice pattern was completed by using already made Somato- measurer, compared with existing bodice pattern, and the results are as follows. The result of the correlation analysis by body measurement shows that chest circumference has a relation to B$.$P-front neck point, side neck point, shoulder point, front interscye breadth point, and the item in spine scapulae point has relation to the item of back neck line, and front & back horizontal values. The degree of shoulder slant, width of armhole and of its depth, the amount of breast, back space, back length were shown to be directly measured from the body. In surface development pattern, tight-fit bodice pattern necessary to the breast volume and back space were shown to be investigated and these volume have to be given in setting up basic line for clothes design together with body measurement value. The result of sensory evaluation for appearance test on fitness shows higher value of research bodice including line of shoulder line, front and back interscye breadth, chest circumference, waist circumference, armhole circumference and of its depth, compared with the research bodice in most items. The result of this study is seen showing high effectiveness for the basic data to design the ready-made dress of high sensitivity of high value added tat.

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충격파 및 유동점성 효과를 고려한 항공기 날개-동체 형상에 대한 공탄성 응답 (Aeroelastic Response Analysis for Wing-Body Configuration Considering Shockwave and Flow Viscous Effects)

  • 김동현;김유성;황미현;박강균
    • 한국항공우주학회지
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    • 제37권10호
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    • pp.984-991
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    • 2009
  • 본 연구에서는 충격파 및 유동박리효과를 고려하여 항공기 동체-날개 형상(DLR-F4)에 대한 천음속 공탄성 응답해석을 수행하였다. 시간 영역에서 전산유체역학, 유한요소모델 및 전산구조동역학 기법을 활용한 유체-구조 연계시스템을 적용하여 공탄성 해석을 수행 하였으며, 이를 이용하여 비행체의 설계에 정확하고 유용한 결과를 제시할 수 있다. 천음속 영역에서 항공기 동체-날개 형상에 대해 비선형 비정상 공력해석을 수행하기 위하여 6면체 구조 격자를 생성하였고, Navier-Stokes 방정식을 적용하였다. 항공기 동체-날개 형상의 정적 및 동적 공탄성 응답 특성을 파악하였고, 항공기 설계 및 시험 연구자에게 실제적이고 유용한 결과를 제시할 수 있다.

섭동법을 이용한 우주 구조물의 동적 운동 해석 (Dynamic Analysis of Space Structure by Using Perturbation Method)

  • 곽문규;성관제
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 춘계학술대회논문집
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    • pp.674-679
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    • 2005
  • This paper is concerned with the application of perturbation method to the dynamic analysis of space structure floating in space. In dealing with the dynamics of space structure, the use of Lagrange's equations of motion in terms of quasi-coordinates were suggested to derive hybrid equations of motion for rigid-body translations and elastic vibrations. The perturbation method is then applied to the hybrid equations of motion along with discretization by means of admissible functions. This process is very tiresome. Recently, a new approach that applies the perturbation method to the Lagrange's equations directly was proposed and applied to the two-dimensional floating structure. In this paper, we propose the application of the perturbation method to the Lagrange's equations of motion in terms of quasi-coordinates. Theoretical derivations show the efficacy of the proposed method.

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다니엘 리베스킨트의 건축 공간 개념에 관한 현상학적 연구 (A Phenomenological Study on the concept of Daniel Libeskind's Architectural Space)

  • 정인하;김홍수
    • 건축역사연구
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    • 제11권1호
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    • pp.33-48
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    • 2002
  • The purpose of this study is to analyze the Daniel Libeskind' spatial concept in view of the Merleau-Ponty's Phenomenology. After the coming of postmodern architecture, the concept of space ceased to be discussed between architects. Instead a sign and a form were supposed as much more important subject to define architectural discipline. But after 1980, the new concept of architectural space was experimented by the architects like Frank Gehry, Peter Eisenman, Steven Hall, and Bernard Tschumi, which was clearly distinguished from modern spatial concept. By the Daniel Libeskind' architecture, this study are to make clear this tendency. For this, we accept as an important instrument Meleau-Ponty's phenomenology and the spatial concept of Minimalism, which stress the relationship of inter-subjectivity between space and human body. Consequently, Daniel Libeskind' spatial concept is characterized by fragmental, accidental, heterogeneous space by accidental events which is occurred by movement of human, which was indentified with Merleau-Ponty's spatial concept.

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현대패션에 나타난 러시아구성주의 건축공간의 중첩연구 (Superimposition of Russian Constructivist Architectural Spaces Reflected in Modern Fashion Design)

  • 진경옥
    • 복식
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    • 제59권9호
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    • pp.163-179
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    • 2009
  • The superimposition of the Russian constructivist architectural design is one of the notable transforming techniques of conventional design principles. The main objective of this paper is to analyse the superimposed space in the modern fashion design based on the techniques and characteristics of superimposition appeared in Russian constructivism architectural space. The artistic characteristics of the superimposed design in the modern fashion design can be determined by codes of dynamics, sense of space, rhythmical sense, communications and tension of the dress. Through this study, it was found that superimposition of the Russian constructivist architectural design in the modern fashion design has influenced the modern fashion design space in the forms of dynamics with directive sense, vitality through transparency, uniformity with geometric interpenetrates, intensive visual attraction created by duplicity, communication between human body and clothes, creation of transformative beauty and enhancement of structural volume on clothes.