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내부자유도를 갖는 차분래티스볼츠만 모델에 의한 에지톤의 수치계산

Numerical Simulation of Edge Tone by Finite Difference Lattice Boltzmann Model with Internal Degree of Freedom

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키워드

주제분류기계공학

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Abstract

A lattice BGK model based on a finite difference scheme with an internal degree of freedom is employed and it is shown that a diatomic gas such as air is successfully simulated. In a weak compressive wave problem and Coutte flow, the validity and characteristics of the applied model are examined. With the model, furthermore, we present a 2-dimensional edge tones to predict the frequency characteristics of discrete oscillations of a jet-edge feedback cycle by the FDLB model (I.D.F FDLBM) in which any specific heat ratio can be chosen freely. The jet is chosen long enough in order to guaranteed the parabolic velocity profile of a jet at the outlet, and the edges have of an angle of and . A sinuous instability wave with real frequency resulting from periodic oscillation of the jet around the edge is propagated on the upper and lower of wedge.

참고문헌 (12)

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  2. "Recent Advances in Lattice Boltzmann Computing" (1995)
  3. "Physical Symmetry and Lattice Symmetry in the Lattice Boltzmann Method", 55, pp.21~24 (1997)
  4. "Proposal of Lattice BGK Model with Internal Degrees of Freedom in Lattice Boltzmann Method", 65(629), pp.92~99 (1999)
  5. "Simulations of Compressible Flows by Using the Lattice Boltzmann and the Finite Difference Lattice Boltzmann Methods", 11(1), pp.489~493 (2003)
  6. "Numerical Simulation of Shock Wave Propagation Using the Finite Difference Lattice Boltzmann Method", 16(10), pp.1327~1335 (2002)
  7. "Sound Generation by a Two-Dimensional Circular Cylinder in a Uniform Flow", 471, pp.285~314 (2002)
  8. "Fluid Mechanics of the Edgetone", 62 no. 5, pp.1116~1128 (1977)
  9. "Vortex-Body Interaction", 30, pp.199~229 (1998)
  10. "Consequence of Edge Oscillations", 39, pp.865~876 (2001)
  11. "On Implementation of the Finite Difference Lattice Boltzmann Method with Internal Degree of Freedom to Edgetone", 19(11), pp.2032 2005~2039
  12. "Computation of Aerodynamic Sounds at Low Mach Numbers Using Finite Difference Lattice Boltzmann Method", 10, pp.8~15 (2005)

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