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깊은 수심을 전파하는 파랑해석해 (Analytical Wave Solution Propagating over Deeper Water)

  • 정태화
    • 한국콘텐츠학회:학술대회논문집
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    • 한국콘텐츠학회 2010년도 춘계 종합학술대회 논문집
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    • pp.633-634
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    • 2010
  • 축대칭 함몰지형 위를 진행하는 확장형 완경사 방정식의 해석해를 유도하였다. 변수분리법을 이용하여 지배방정식을 상미분방정식으로 만들었으며, 파속과 군속도로 표현되는 계수들은 Hunt(1979)의 근사식을 이용하여 양함수의 형태로 표현하였다. 마지막으로 Frobenius기법을 이용하여 확장형 완경사방정식의 해를 유도하였다.

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조선왕조대의 칭법과 필법

  • 류인영
    • 한국수학사학회지
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    • 제13권2호
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    • pp.23-32
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    • 2000
  • Using some units of length, weight and time, human beings have constructed their own cultures in many regions on earth. This paper aims to study the applied methods of Ching and Pil, i.e. the units of length and weight in the Chosun dynasty and to investigate their meanings.

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구 주위의 비정상 면대칭 및 비대칭 유동의 특성 (CHARACTERISTICS OF UNSTEADY PLANAR-SYMMETRIC AND ASYMMETRIC FLOWS OVER A SPHERE)

  • 김동주
    • 한국전산유체공학회지
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    • 제13권4호
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    • pp.39-44
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    • 2008
  • Numerical simulations of laminar flow over a sphere are conducted to investigate the effect of the Reynolds number on the characteristics of vortex shedding. The Reynolds numbers considered are between 300 and 475, covering unsteady planar-symmetric and asymmetric flows. Results show that the unsteady planar-symmetric flow can be categorized into two different regimes: single-frequency regime and multiple-frequency regime. The former has a single frequency component due to periodic shedding of the vortices with the same strength in every shedding cycle, while the latter has multiple frequency components due to cycle-to-cycle variation in the strength of shed vortices with the shedding angle fixed. The multiple-frequency planar-symmetric flow, which is newly found in the present study, occurs at Re=330${\sim}$360 between the single-frequency planar-symmetric flow and the asymmetric flow. On the other hand, the asymmetric flow occurs at Re${\geq}$365, where the vortices shed from the sphere show variation both in strength and shedding angle unlike the planar-symmetric flow. Also, it is shown that the breaking of planar symmetry is closely related to the imbalance of vortical strength between a pair of streamwise vortices.

점탄성 원통의 모드 I 균열 해석 (Numerical Analysis of Viscoelastic Cylinders with Mode I Cracks)

  • 심우진;오근
    • 한국전산구조공학회논문집
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    • 제19권3호
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    • pp.259-269
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    • 2006
  • 원환균열과 원주균열을 지닌 축대칭 선형 점탄성 중실축과 중공축이 외력을 받을 때 파괴역학 변수로서 응력확대계수, 에너지방출률 그리고 균열개구변위의 수치해를 유한요소해법을 이용하여 구한다. 균열선단에서는 응력의 특이성을 지닌 1/4절점 삼각형 특이요소가 사용된다. 또한 수치해를 비교 검증하기 위해 탄성-점탄성 상응원리를 이용하여 선형파괴역학의 탄성해들로부터 점탄성 이론해가 유도 제시된다. 해석에 사용되는 점탄성 물성은 체적변형은 탄성적이고 전단변형은 표준선형고체처럼 거동한다고 가정한다. 제시된 수치해법과 이론해는 축대칭 점탄성 거동 연구에 중요한 자료가 된다.

역대칭(逆対称) Cross-ply 다층판(多層板)의 자유진동(自由振動) 및 변형 에너지 해석(解釋) (Free Vibrations and Strain Energy Anaylsis of Antisymmetric Cross-ply Laminted Plates)

  • 박문호;진 요시무라;타카시 미카미;박승진
    • 대한토목학회논문집
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    • 제11권4호
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    • pp.37-44
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    • 1991
  • 두 변이 단순지지된 역대칭 cross-ply 다층판의 자유진동에 대하여 Yang, Norris, Stavsky의 YNS 이론을 이용하여, 다층판의 자유진동해석과 변형에너지 해석을 하였다. 다층판의 운동방정식은 선점법을 이용하여 해석하였고, 탄성계수비와 적층수가 고유진동수에 미치는 영향을 검토하였다. 또한 변형에너지 분포해석을 이용하여 다층판의 진동특성을 명확히 규명하였다.

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원관 내의 디스크를 지나는 축대칭 스톡스 유동 (AXISYMMETRIC STOKES FLOW PAST A DISK IN A CIRCULAR TUBE)

  • 정재택
    • 한국전산유체공학회지
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    • 제21권4호
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    • pp.96-101
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    • 2016
  • A two-dimensional Stokes flow past a circular disk in a circular tube is analyzed. The circular disk is located coaxially with the circular tube and the Hagen-Poiseuille flow exists at upstream and downstream far from the circular disk. The Stokes approximation is used and the flow is investigated analytically by using the method of eigenfunction expansion and the method of least square. From the analysis, the stream function and the pressure of the flow field are obtained, and the streamlines and pressure distribution are shown. Also, the pressure and shear stress distributions on the circular disk and circular tube wall are calculated, and shown for some typical radii of the circular disk. The additional pressure drop induced by the disk and the drag force exerted on the disk are compared as functions of the radius of the circular disk, and it is shown that the shear force on the wall of the tube increases due to the disk.

축대칭 하향단흐름에서 자유흐름 난류강도의 영향 (Effects of the free Stream Turbulence Intensity on the Flow Over an Axisymmetric Backward-Facing Step)

  • 양종필;김경천;부정숙
    • 대한기계학회논문집
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    • 제19권9호
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    • pp.2328-2341
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    • 1995
  • An experimental study on the flow over the axisymmetric backward-facing step was carried out. The purposes of the present study are to investigate the effect of the free stream turbulence intensity on the reattachment length and to understand the turbulence structure of the recirculating flows. Local mean and fluctuating velocity components were measured in the separated and reattaching axisymmetric turbulent boundary layer over the wall of convex cylinder placed in a water tunnel by using 2-color 4-beam fiber optics laser Doppler velocimetry. As the free stream turbulence intensity increased, the reattachment length became shorter due to the enhanced mixing in the separated shear layer. It was also observed that the reverse flow velocity and turbulent kinetic energy increase with increasing free stream turbulence intensity. Spectral data and flow visualization showed that low-frequency motions occur in the separated flow behind a backward-facing step. These motions have a significant effect on the time-averaged turbulence data.

SM45C 강의 변형제어를 위한 열처리기술에 관한 연구 (A Study on the Heat-treatment Technique for Deformation Control of SM45C steel)

  • 류성기;남태현;박준철
    • 한국정밀공학회지
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    • 제18권4호
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    • pp.78-84
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    • 2001
  • This study deals with the heat-treatment technique of SM45C steel with respect to less of deformation in control. The whole process for the production of landing gear must go through with uniformally controlled heat treatment, where as most deformation usually occur in nonuniform cooling environment. When a heated metal is submerged into a certain quenchant, the rate of cooling rapidity can be measured rather slow during the early stage of the procedure due to an Occurrence of a vapor blanked. As the additional course of cooling action is applied and the vapor from a vapor blanked is destroyed simultaneously, the speed of cooling promptness can be considered rather swift. The object of this study is to control the certain deformations as in the procedure of a heat treatment for landing gear by analyzing and improving the conditions of different substance of quenching liquids. Several noticeable curves indicating the temperature variation on the ap-plied metals during the cooling procedures, along with detectable rates of water verses oil and that of different polymer solutions are illustrated.

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