• 제목/요약/키워드: space of flow

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정서 차원 공간에서 소설의 지배 정서 분석 및 분류 (Analyzing and classifying emotional flow of story in emotion dimension space)

  • 이신영;함준석;고일주
    • 인지과학
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    • 제22권3호
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    • pp.299-326
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    • 2011
  • 소설, 블로그, 채팅 메시지, 상품평 등의 텍스트는 전반적인 정서의 흐름을 가지고 있다. 텍스트 간의 정서 흐름의 유사도를 비교하면 유사한 정서 흐름을 갖는 텍스트를 분류할 수 있고, 상품 추천이나 의견 수집 등에 활용할 수 있다. 본 논문에서는 텍스트에서 정서 단어를 순차적으로 추출하고 쾌-불쾌, 활성화의 2차원으로 분석하여 텍스트의 정서 흐름을 파악하였다. 또한 텍스트의 순차적인 흐름을 시간 차원으로 설정하여 텍스트의 전반적인 정서 흐름인 '지배 정서(dominant emotion)'를 파악하기 위하여 쾌-불쾌, 활성화, 시간의 3차원 공간에서 정서 흐름을 탐색하였다. 또한 이 3차원 공간 안에서 유클리드 거리를 사용하여 지배 정서 흐름의 유사도를 계산함으로써 유사한 정서 흐름을 가지는 텍스트를 분류하는 방법을 제안하였다. 제안한 방법을 통해 한국 근대 단편 소설들을 분석하여 지배 정서를 분석하였고 유사한 지배 정서를 가지는 소설들을 분류하였다.

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Experimental and Computational Study on Separation Control Performance of Synthetic Jets with Circular Exit

  • Kim, Minhee;Lee, Byunghyun;Lee, Junhee;Kim, Chongam
    • International Journal of Aeronautical and Space Sciences
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    • 제17권3호
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    • pp.296-314
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    • 2016
  • This paper presents experimental and computational investigations of synthetic jets with a circular exit for improving flow control performance. First, the flow feature and vortex structure of a multiple serial circular exit were numerically analyzed from the view point of flow control effect under a cross flow condition. In order to improve separation control performance, experimental and numerical studies were conducted according to several key parameters, such as hole diameter, hole gap, the number of hole, jet array, and phase difference. Experiments were carried out in a quiescent condition and a forced separated flow condition using piezoelectrically driven synthetic jets. Jet characteristics were compared by measuring velocity profiles and pressure distributions. The interaction of synthetic jets with a freestream was examined by analyzing vortical structure characteristics. For separation control performance, separated flow over an airfoil at high angles of attack was employed and the flow control performance of the proposed synthetic jet was verified by measuring aerodynamic coefficient. The circular exit with a suitable hole parameter provides stable and persistent jet vortices that do beneficially affect separation control. This demonstrates the flow control performance of circular exit array could be remarkably improved by applying a set of suitable hole parameters.

노즐 위치 및 분사각이 공기유동 및 $CO_2$ 소화제 전달특성에 미치는 영향 (The Effect of Nozzle's Location & Injection Angle on the Characteristics of Air Flow and $CO_2$ Extinguishant Transfer)

  • 박찬수
    • Journal of Advanced Marine Engineering and Technology
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    • 제26권4호
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    • pp.472-484
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    • 2002
  • To analyze the characteristics of air flow and $CO_2$ extinguishant transfer when extinguishant is injected into a closed space similar to marine engine room, a numerical simulation on a space was performed. Flow fields and $CO_2$ concentration fields are calculated according with the variation of the location & injection angle of nozzles. The results of simulation showed that the pattern of recirculation flow was affected greatly with the location & injection angle of nozzles and such a recirculation flow accelerated mass transfer of $CO_2$ and greatly affected the diffusion process of $CO_2$ extinguishant. It is considered that this result of this study can be useful to designing the arrangement of nozzles for the $CO_2$ fire fighting equipments in a marine engine room.

Sensitivity analysis of transonic flow past a NASA airfoil/wing with spoiler deployments

  • AKuzmin, lexander
    • International Journal of Aeronautical and Space Sciences
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    • 제15권3호
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    • pp.232-240
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    • 2014
  • Transonic flow past a NASA SC(2)-0710 airfoil with deployments of a spoiler up to $6^{\circ}$ was studied numerically. We consider angles of attack from $-0.6^{\circ}$ to $0.6^{\circ}$ and free-stream Mach numbers from 0.81 to 0.86. Solutions of the unsteady Reynolds-averaged Navier-Stokes equations were obtained with a finite-volume solver using several turbulence models. Both stationary and time-dependent deployments of the spoiler were examined. The study revealed the existence of narrow bands of the Mach number, angle of attack, and spoiler deflection angle, in which the flow was extremely sensitive to small perturbations. Simulations of 3D flow past a swept wing confirmed the flow sensitivity to small perturbations of boundary conditions.

Control of Delta-Wing Vortex by Apex Strake

  • Sohn, Myong-Hwan;Chung, Hyoung-Seog
    • International Journal of Aeronautical and Space Sciences
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    • 제8권2호
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    • pp.98-106
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    • 2007
  • The vortex flow characteristics of a double-delta wing, which can change the incidence angle of its apex strake was investigated through the wing-surface pressure measurement and the particle image velocimetry(PIV) measurement of the wing-leeward flow region. The apex strake has sharp edges and can change its incidence angle with a hinge line at the 23% chord position measured from the apex of the main wing. The present study revealed that the incidence-angle change of the apex strake could greatly alter the vortex flow pattern around the double-delta wing and the wing-surface pressure distribution, which suggested that the apex strake could be used as an effective device for the active control of delta-wing vortex flow.

Control of Delta-Wing Vortex by Micro-Fin-Type Leading-Edge Flap

  • Sohn, Myong-Hwan;Chung, Hyoung-Seog;Cho, Dong-Hyun
    • International Journal of Aeronautical and Space Sciences
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    • 제7권2호
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    • pp.128-136
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    • 2006
  • The present study examined the effects of micro leading-edge flaps on the vortex characteristic changes of a double-delta wing through pressure measurements of the wing upper surface and PIV measurements of the wing-leeward flow region. The experimental data were collected and analyzed while changing the deflection angle of the leading-edge flaps to investigate the feasibility of using micro leading-edge flaps as flow control devices. The test results revealed that the leading edge modification could greatly alter the vortex flow pattern and the wing surface pressure of the delta wing, which suggested that the leading-edge flaps could be used as an effective device for the control of delta-wing vortex flow.

공업고등학교(工業高等學校) 실습실(實習室)의 공간(空間) 구성(構成)에 관한 조사연구(調査硏究) - 건축(建築)과 실습실(實習室)을 중심(中心)으로 - (A Survey Study on the Space in Technical High-School - Focused on the Department of Architecture -)

  • 남궁의;김상겸
    • 교육시설
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    • 제7권2호
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    • pp.5-13
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    • 2000
  • In order to make good educational circumstance of the Technical High-school, it is important that we must aware of the characteristics of technical high-school and take all considerations into the planning. This study is to plan the architectural space and path of flow in practice rooms through questionnare survey. The result are as follow. A majority of respondents recognize that the existing facility and space condition are not appropriate, because the past investment has overemphasized on the quantitative aspect. It is time to need the change of its directions toward the quantitative investment in future. It is also necessary to plan the space and the path of flow of the practice rooms in consideration of the characteristics of school.

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원심압축기 채널디퓨저 내부의 압력분포에 관한 연구 (A Study on Pressure Distributions in a Centrifugal Compressor Channel Diffuser)

  • 강정식;강신형
    • 대한기계학회논문집B
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    • 제25권4호
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    • pp.507-513
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    • 2001
  • Time averaged pressure distributions in a high-speed centrifugal compressor channel diffuser at design and off-design flow rates are investigated. Pressure distributions from the impeller exit to the channel diffuser exit are measured for various flow rates from choke to near surge condition, and the effects of operating condition are discussed. The strong non-uniformity in the pressure distribution is obtained over the vaneless space and semi-vaneless space caused by the impeller-diffuser interaction. As the flow rate increases, flow separation near the throat, due to large incidence angle at the vane leading edge, increases aerodynamic blockage and reduces the aerodynamic flow area downstream. Thus the minimum pressure location occurs downstream of the geometric throat, and it is named as the aerodynamic throat. And at choke condition, normal shock occurs downstream of this aerodynamic throat. The variation in the location of the aerodynamic throat is discussed.

투명성 효과를 위한 재료의 특성 및 적용 방법 (An Analysis of Application of Transparent Materials in Interior Space)

  • 정필영
    • 한국디지털건축인테리어학회논문집
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    • 제7권2호
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    • pp.19-24
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    • 2007
  • This study attempts to examine and to analyze the characteristics of transparent materials and its methods to apply in space. the ability to see through a physical element, whether it is clear glass, sandblasted acrylic, or a delicate fabric, can have a dramatic and sensory effect on the overall perception of a space. The various range of Transparent materials and product in glass, plastic, fabric, and grid now gives us the potential to maximize the flow of light in our enclosed space. This research will explore how transparent, translucent, and semi-opaque elements can be used within the interior with full range of see-through materials. The transparent materials can be divided in two level - as structural elements and as stylish accessories. A glass partition or floor, metal mesh stairs can create divisions or link one space to another while maintaining effective levels of natural light. there is also various level of products from glass chair to basin. With the enthusiasm for using transparent materials, transparent materials will be more decorative and powerful application while still maximize the highest possible flow of light.

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