• 제목/요약/키워드: Transverse flow

검색결과 369건 처리시간 0.026초

Numerical Simulation Study on Combustion Characteristics of Hypersonic Model SCRamjet Combustor

  • Won, Su-Hee;Eunju Jeong;Jeung, In-Seuck;Park, Jeong-Yeol
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.42-47
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    • 2004
  • Air-fuel mixing and flame-holding are two important factors that have to be considered in the design of an injection system. Different injection strategies have been proposed with particular concern for rapid air-fuel mixing and flame-holding. Two representative injection techniques can be applied in a supersonic combustor. One of the simplest approaches is a transverse(normal) injection. The cavity flame holder, an integrated fuel injection/flame-holding approach, has been proposed as a new concept for flame holding and air-fuel mixing in a supersonic combustor. This paper describes numerical efforts to characterize the flame-holding and air-fuel mixing process of a model scramjet engine combustor, where hydrogen is injected into a supersonic cross flow and a cavity. The combustion phenomena in a model scramjet engine, which has been experimentally studied at University of Queensland and Australian National University using a free-piston shock tunnel, were observed around the separation region of the transverse injector upstream and the inside cavity. The results show that this flow separation generates recirculation regions which increase air-fuel mixing. Self-ignition occurs in the separation-freestream and cavity-fteestream interfaces.

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만곡부 혼합입경 하상횡경사 모형의 개발 (Development of Transverse Bed Slope Model for Nonuniform Sand Bed at River Bend)

  • 최종인;고재웅
    • 물과 미래
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    • 제29권4호
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    • pp.177-186
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    • 1996
  • 하천 만곡부에서의 하상 횡경사 결정은 유수와 유수의 소류력에 의해 변동하는 하상면과의 상호관계를 규명하는 이론적인 접근에서 출발하게 된다. 이러한 경우 흐름은 완전히 발달한 흐름으로 해석하게 되며 하상에서는 소류사가 일어나고 있는 상태에서 유수력과 하상물질에 의한 저항력간의 평형을 바탕으로 해석을 시도하게 된다. 한계소류력을 대표하는 연구로서 Shields diagram이 많이 이용되고 시동조건으로 Shields parameter를 0.06으로 대표해 주고 있다. 지금까지 만곡부의 하상횡경사 결정에서는 대부분의 방법들이 Shields parameter 의 적용에서 0.06을 일률적으로 채택하고 있다. 본 연구에서는 Shields parameter에서의 실험조건인 균일입경하상이라는 조건이 적용되지 않는 일반 자연하천에서 혼합입경하상의 입도분포곡선 형태에 따라 생기는 Shields parameter의 변동을 고려할 수 있도록 하므로써 보다 정확한 만곡부 하상횡경사 추정이 가능한 방법을 제시하였다.

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유로만곡부의 횡방향 하상경사 산정 모형에 관한 연구 (A Study on Selected Transverse Bed Slope Models in Channel Bend)

  • 송재우;최인호;김지호
    • 대한토목학회논문집
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    • 제14권6호
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    • pp.1395-1404
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    • 1994
  • 유로만곡부의 횡방향 하상경사는 하천형태학적 특성연구와 하도재해방지, 그리고 수공구조물 보호 등에 기초자료를 제공하는 중요한 연구과제이다. 본 연구에서는 연구대상유역 유로만곡부의 횡방향 하상경사를 Odgaard의 모형외 8개의 모형을 선택하여 비교분석한 후 예측하였으며 적합한 모형을 제시하였다. 본 연구에서 비교된 모든 모형들은 곡률반경과 수심에 비례하였고 모형들사이의 차이는 비례계수 K에 있으며 또한 측정된 횡방향 하상경사는 만곡부에서의 최대수심과 평균유속, 그리고 입자 Froude수와 관계가 있었다. 본 연구에서 Sacramento강 만곡부에서 이루어진 Odgaard의 실험자료를 이용하여 횡방향 하상경사모형들을 비교분석한 결과 Odgaard89모형이 실측횡방향 하상경사와 비교적 잘 일치하였다.

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두 이동질량이 단순지지 유체유동 파이프의 동특성에 미치는 영향 (Influence of Two Moving Masses on Dynamic Behavior of a Simply Supported Pipe Conveying Fluid Flow)

  • 윤한익;임순홍;유진석
    • 한국소음진동공학회논문집
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    • 제13권8호
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    • pp.605-611
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    • 2003
  • A simply supported pipe conveying fluid and two moving masses upon it constitute this nitration system. The equation of motion is derived by using Lagrange's equation. The influence of the velocities of two moving masses, the distance between two moving masses, and the velocities of fluid flow in the pipe have been studied on the dynamic behavior of a simply supported pipe by numerical method. The velocities of fluid flow are considered with in its critical values of a simply supported pipe without moving masses upon It. Their coupling effects on the transverse vibration of a simply supported pipe are inspected too. As the velocity of two moving masses increases, the deflection of a simply supported pipe is increased and the frequency of transverse vibration of a simply supported pipe is not varied. In case of small distance between two masses, the maximum deflection of the pipe occur when the front mass arrive at midspan. Otherwise as the distance get larger, the position of the front masses where midspan deflection is maximum moves beyond the midpoint of a simply supported pipe. The deflection of a simply supported pipe is increased by coupling of the velocities of moving masses and fluid flow.

PIV measurements of near wake behind a sinusoidal cylinder

  • Zhang W.;Daichin Daichin;Lee S. J.
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2003년도 추계학술대회 논문집
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    • pp.59-62
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    • 2003
  • The near wake behind a sinusoidal cylinder at Re=5200 has been investigated using DPIV system. The velocity fields, streamlines and vorticity contours of the mean flow were compared at the nodal, saddle and middle planes with those of a right circular cylinder. For the sinusoidal cylinder, the vortex core moves downstream and the vortex formation region is expanded in streamwise direction while suppressed in transverse direction at the nodal plane. At the saddle and the middle plane the vortex spread in both streamwise and transverse directions, forming the maximum vortex region at the saddle plane.

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부정류 모의 기반 오프라인 저류지 조성에 따른 홍수위 변화 민감도 분석 (Sensitivity Analysis on Flood Level Changes by Offline Storage Creation Based on Unsteady Flow Modeling)

  • 장은경;지운;김상혁;류지원
    • Ecology and Resilient Infrastructure
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    • 제10권4호
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    • pp.217-225
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    • 2023
  • 본 연구에서는 금강 장동지구를 대상으로 홍수완충공간을 오프라인 저류지로 조성하여 운영하는 경우에 대해 홍수위 저감 효과를 1차원 부정류 수치모의를 통해 분석하였다. 특히 오프라인 저류지의 횡월류 위어 높이와 폭 (길이)의 변화에 따른 수위변화의 민감도를 분석하여 홍수관리시설 (제방) 설계에 필요한 정보를 정량적으로 제공하였다. 첨두 홍수량 및 홍수위를 기준으로 오프라인 저류지의 홍수조절효과를 분석한 결과, 공간적으로는 홍수완충공간 조성 예정지와 하류구간에서 홍수조절효과가 확인되었으며, 특히 하류에서 가장 큰 홍수저감 효과가 나타나는 것을 확인할 수 있었다. 횡월류 위어의 설계 조건별로는 50년 빈도 홍수위 기준의 월류고와 125 m의 횡월류 위어 폭 (길이)을 고려한 조건에서 가장 큰 홍수저감 효과가 나타났다. 오프라인 저류지 조성으로 최대홍수량 도달 시간이 지연되는 효과 또한 부정류 모의를 통해 제시하였다.

축대칭 하향단 흐름에 대한 실험적 연구 (Experimental Study on the Flow Behind an Axisymmetric Backward-Facing Step)

  • 김경천;부정숙;양종필
    • 대한기계학회논문집
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    • 제18권9호
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    • pp.2463-2476
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    • 1994
  • Local mean fluctuating velocity components were measured in the separating and reattaching axisymmetrc region of turbulent boundary layer over the wall of convex cylinders placed in a water tunnel by using 2-color 4-beam fiber optics laser Doppler velocimetry. Measurements were made with three different diameters of cylinders with four different diameters of cylinders with four different diameter of the obstructions. The range of Reynolds number based on step height was between 5,000 to 25,200. The study demonstrates that the reattachment length decreases with decreasing cylinder radius and is always shorter than that for the two-dimensional backward-facing step flow at the condition of the same step height. It was also observed that the turbulent kinetic energy in the recirculating region increases with an increases in the radius of convex curvature. The measured velocity field suggests that the transverse curvature can effect definitely the formation of corner eddy.

Space-Time Characteristics of the Wall Shear-Stress Fluctuations in an Axial Turbulent Boundary Layer with Transverse Curvature

  • Shin, Dong-Shin;Lee, Seung-Bae;Na, Yang
    • Journal of Mechanical Science and Technology
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    • 제19권8호
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    • pp.1682-1691
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    • 2005
  • Direct numerical simulation database of an axial turbulent boundary layer is used to compute frequency and wave number spectra of the wall shear-stress fluctuations in a low-Reynolds number axial turbulent boundary layer. One-dimensional and two-dimensional power spectra of flow variables are calculated and compared. At low wave numbers and frequencies, the power of streamwise shear stress is larger than that of spanwise shear stress, while the powers of both stresses are almost the same at high wave numbers and frequencies. The frequency/streamwise wave number spectra of the wall flow variables show that large-scale fluctuations to the rms value is largest for the stream wise shear stress, while that of small-scale fluctuations to the rms value is largest for pressure. In the two-point auto-correlations, negative correlation occurs in streamwise separations for pressure, and in span wise correlation for both shear stresses.

초음속난류유동장에서 후향계단 후류의 측면제트분사에 대한 수치적 연구 (Numerical Study of slot injection behind a rearward-facing step into turbulent supersonic flow)

  • 김종록;김재수
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2002년도 춘계 학술대회논문집
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    • pp.17-22
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    • 2002
  • This paper describes numerical research on transverse jet behind rearward-facing step in turbulent supersonic flowfields without chemical reaction. The purpose of transverse jet behind rearward-facing step is to improve mixing of the fuel in the combustor. Two-dimensional unsteady flowfields generated by slot injection into supersonic flow are numerically simulated by integration of Navier-Stokes equation. Final-scale turbulence effects are modeled with two-equation $\kappa-\epsilon$ model. Numerical methods are modeled high-order upwind TVDschemes. A total of 4 cases are computed, comprising slot momentum flux ratios at four step heights downstream of the step. These numerical results are represented periodic phenomenon in unsteady flowfields.

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