• Title/Summary/Keyword: Inflection Angle

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Numerical Study on an E-D Nozzle Characteristics with Various Pintle Inflection Angles (핀틀 변곡 각도에 따른 E-D 노즐 특성에 대한 전산수치해석 연구)

  • Park, Sanghyeon;Moon, Taeseok;Huh, Hwanil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.6
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    • pp.19-27
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    • 2018
  • In this study, a numerical study was conducted to characterize the E-D nozzle which changes according to the nozzle pressure ratios. Three different numerical analysis models were designed by changing the pintle inflection angles. When the nozzle pressure ratio is low, the outside air flows into the E-D nozzle to form an open flow field. As the nozzle pressure ratio increases, the flow transition occurs to become the closed flow field where the recirculation region is isolated inside the nozzle. Also, the highest thrust coefficient was obtained in the analytical model with high pintle inflection angle at all nozzle pressure ratios.

Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed (팽창비가 고정된 듀얼 벨 노즐의 천이특성에 대한 수치해석 연구)

  • Choi, Junsub;Huh, Hwanil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.3
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    • pp.68-75
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    • 2017
  • Dual bell nozzle is a type of altitude compensation nozzle, which is a nozzle that minimize the losses of the specific impulse at the off-design point of a typical bell nozzle. In this paper, numerical computations are performed to understand the transition characteristics of dual bell nozzles with fixed expansion ratios. The major design variables are the length of extension and the angle of inflection. As the length of the extension increased, the transition altitude and transition duration increased and the reduction of the thrust coefficient decreased. As the angle of inflection increased, the transition altitude and transition duration decreased and the reduction of the thrust coefficient increased.

An Analytic Solution of the Shape of an Inclined, Partially Filled Membrane Container (경사면에 놓인 유체 저장용 막구조물 형상의 이론적 해석)

  • Choi, Yoon-Rak
    • Journal of Ocean Engineering and Technology
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    • v.21 no.1 s.74
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    • pp.45-50
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    • 2007
  • For a long partially-filled membrane container on an incline, the analytic solution of the similarity shape is studied. The nonlinear equation is solved and its solution is expressed as elliptic integrals, which include an unknown at the point of inflection. The point of inflection is determined by using the boundary condition at the upper separating point. Some characteristic values of the universal shape are evaluated, as the functions of inclination angle and shapes are illustrated for some cases.

Damage Assessment of Buried Pipelines Due to Tunnelling (터널 굴착에 의한 지중 매설관의 손상평가)

  • 유충식;윤효석
    • Proceedings of the Korean Geotechical Society Conference
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    • 2000.11a
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    • pp.471-478
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    • 2000
  • Ground movements are inevitably caused by tunnel construction in soft ground. In the design and construction of tunnels in urban areas, the potential effects of buried pipelines by ground movements are one of the important design cosiderations. Generally, the most common modes of failure of buried pipelines due to ground movements are tensile fracture of main pipelines, rotation angle and pull-out displacement at joints. In the parametric study, a wide range of conditions were considered, including tunnel diameter(D), tunnel depth(Z$\sub$0/), volume loss(V$\sub$ι/) and inflection point(i). Based on this results, design charts, which are applicable to assess potential damage of buried pipelines associated ground movements due to tunnelling, are developed.

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A Study on the Wind Pressure Coefficients of Flat-type Apartment Complexes Considering Building Layout and Aspect Ratio (판상형 공동주택의 동 배치 및 종횡비에 따른 풍압계수 특성에 관한 연구)

  • Yoon, Seong-Hoon
    • Journal of the Korea Convergence Society
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    • v.12 no.9
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    • pp.153-159
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    • 2021
  • In this study, basic data that can be referenced for ventilation modeling was presented by analyzing the characteristics of wind pressure coefficients(Cp) according to wind direction angles under conditions of different building layouts and aspect ratios through CFD (Computational Fluid Dynamics) analysis for flat-type apartment complexes. In the case of a wind direction angle of 0°, Cp distribution in the form of an inverted S-shape was shown on the front of the building located on the windward side. And Cp corresponding to the lowest floor, the uppermost floor, and the two inflection points showed relatively close values regardless of the height of the building. The inflection point of the low-rise part was formed at a height of about 11m, and the height of the high-rise part could be calculated through a trend formula proportional to the height of the building. It was confirmed that the averaged Cp value can be applied in most conditions except for the wind direction angle of 45 degrees.

An Experimental Study on the Flow Characteristics with the Impinging Angles of Defrost Nozzle Jet Inside a Vehicle Passenger Compartment (차실내 Defrost 노즐 분류의 충돌각 변화에 따른 유동특성에 관한 실험적 연구)

  • Kim, Duck-Jin;Kim, Hyun-Joo;Rho, Byung-Joon;Lee, Jee-Keun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.12
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    • pp.1024-1032
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    • 2007
  • The flow characteristics with the impinging angles of defrost nozzle jet inside a commercial vehicle passenger compartment were investigated experimentally by using the two-dimensional duct-nozzle model. The shape of the nozzle contraction was designed according to the curved line of cubic equation to the vertical plan of the flow direction. The impinging angles, defined as the angle between nozzle axis and a vertical line to the windshield, were varied from the $0^{\circ}\;to\;80^{\circ}$. The mean velocity distributions, the half-widths, and the momentum distributions with the cases of both the free jet and the impinging jet onto the dummy windshield were measured. The impinging jet flows similarly with wall jet from $X/b_o=20$, and the impinging angle has an effect on the half-width of the impinging jet. The momentum distributions onto the windshield increased with the increase of impinging angle, and then their inflection point was observed around the impinging angle of $60^{\circ}$.

Characteristics and Key Parameters of Dual Bell Nozzles of the DLR, Germany (독일 DLR의 듀얼 벨 노즐 특성 및 핵심 변수)

  • Kim, Jeonghoon;Huh, Hwanil
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.11
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    • pp.952-962
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    • 2015
  • Various types of altitude compensation nozzles have been investigated to develop an effective propulsion system. In order to obtain baseline data for future study of dual bell nozzles, main characteristics and key parameters of dual bell nozzles are summarized and described by analysing DLR dual bell nozzles. DLR's experimental researches show that inflection angle is proportional to transition NPR, and extension length is proportional to side load, but inversely proportional to transition NPR and transition duration. Therefore, the nozzle geometry can be determined through the performance prediction process and thus the optimization process is required to meet performance requirements between parameters.

Optical Characteristics of a Flexible Back-Light Unit with Plasma Discharge Clusters

  • Goo, Gyo-Uk;Ryu, Si-Hong;Lee, Seung-Eui;Ahn, Sung-Il
    • Transactions on Electrical and Electronic Materials
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    • v.12 no.5
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    • pp.189-192
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    • 2011
  • A flexible back-light unit (FBLU) is fabricated by embedding plasma discharge clusters in a flexible polymer matrix. The brightness uniformity of an FBLU was measured for various combinations of optical sheets and compared with the simulated results for various bending angles. A gap between light sources causes distinctive integrated brightness curves which have two inflection points depending on bending angle. The brightness distribution of a simulated BLU was in good agreement with that of an actual plasma BLU except for a dark area that appeared at the center of the simulated BLU. The real and simulated BLUs both clearly showed an angle dependency caused by mirror images located between point light sources. On the basis of these results, it is suggested that these mirror-like images could be a major factor in determining the characteristics of FBLUs.

Optimum Blind Control Considering Characteristics of Solar Profile Angle Curve (건물에서 태양 프로파일의 변화 특성을 고려한 블라인드 최적 제어 방안)

  • Seong, Yoon-Bok
    • Journal of the Korean Solar Energy Society
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    • v.31 no.6
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    • pp.111-124
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    • 2011
  • The objective of this study is to develop the blind control strategy and method which reduce negative effect of incoming daylight on visual comfort of occupants, minimize psychological anxieties caused by frequent motions of a blind, and maximize positive effect of incoming daylight by opening/closing of a blind. In previous researches on blind controls, major problem is that the time interval and amount of blind movement do not meet the control objective at the inflected zone of solar profile curve. To overcome these limitations revealed in theprevious researches, following tasks were performed in this study. i)To establish the control objective to accomplish the goal of this study. ii)To develop the control methods and algorithms which prevent glare on the work-plane at any time and which control the time interval and amount of blind movement to follow the control objective at various solar profile angle curves. This study proposed the control strategy and method that define the base control section implying the inflection point within the control objective zone and subsequently, divide the control sections for the residual time zones. The proposed strategy and method are found to increase the incoming daylight and solar irradiation by 0 to 15 %.

풍력 블레이드의 전단 웹 모양의 최적화를 위한 구조 해석에 대한 연구

  • Kim, Jin-Myeong;Song, Seong-Il
    • Proceeding of EDISON Challenge
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    • 2015.03a
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    • pp.217-222
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    • 2015
  • In this paper, a study was conducted for the optimization through shear web of shape the Edison program in wind power blade. We measured the displacement and stress distribution through two optimization methods to select the model with the smallest displacement and stress values. Before running the analysis, We try to find the inflection point through the shear web of the model and then analyze by introducing the geometric nonlinearity. The first optimization variables are introduced by the pitch angle and three web shapes. Third model such a honeycomb structure is good way to get an advantage for bending test. According to a method of previous optimization, third model is chosen and then the thickness of the web and blade as a variable is introduced, it is extracted as a result of displacement and the maximum stress per mass.

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