• Title/Summary/Keyword: Harten-Lax-van Leer-contact(HLLC)

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Two-phase Finite Volume Analysis Method of Debris Flows in Regional-scale Areas (2상 유한체적모델 기반의 광역적 토석류 유동해석기법)

  • Jeong, Sangseom;Hong, Moonhyun
    • Journal of the Korean Geotechnical Society
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    • v.38 no.4
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    • pp.5-20
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    • 2022
  • To analyze the flow and density variations in debris flows, a two-phase finite volume model simplified with momentum equations was constructed in this study. The Hershel-Buckley rheology model was employed in this model to account for the internal and basal friction of debris flows and was utilized to analyze complex topography and entrainments of basal soil beds. In order to numerically solve the debris flow analysis model, a finite volume model with the Harten-Lax-van Leer-Contact method was used to solve the conservation equation for the debris flow interface. Case studies of circular dam failure, non-Newtonian fluid dam failure, and multiple debris flows were analyzed using the proposed model to evaluate shock absorption capacity, numerical isotropy, model accuracy, and mass conservation. The numerical stability and correctness of the debris flow analysis of this analysis model were proven by the analysis results. Additionally, the rate of debris flow with various rheological properties was systematically simulated, and the effect of debris flow rheological properties on behavior was analyzed.

Numerical Study on Compressible Multiphase Flow Using Diffuse Interface Method (Diffuse Interface Method를 이용한 압축성 다상 유동에 관한 수치적 연구)

  • Yoo, Young-Lin;Sung, Hong-Gye
    • Journal of Aerospace System Engineering
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    • v.12 no.2
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    • pp.15-22
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    • 2018
  • A compressible multiphase flow was investigated using a DIM consisting of seven equations, including the fifth-order MLP and a modified HLLC Riemann solver to achieve a precise interface structure of liquid and gas. The numerical methods were verified by comparing the flow structures of the high-pressure water and low-pressure air in the shock tube. A 2D air-helium shock-bubble interaction at the incident shock wave condition (Mach number 1.22) was numerically solved and verified using the experimental results.