2016
DOI: 10.1017/jfm.2016.47
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A numerical investigation of the wake of an axisymmetric body with appendages

Abstract: We report wall-resolved large-eddy simulations of an axisymmetric body of revolution with appendages. The geometry is that of the DARPA SUBOFF body at 0 yaw angle and a Reynolds number equal to Re L = 1.2 × 10 6 (based on the free-stream velocity and the length of the body). The computational grid, composed of approximately 3 billion nodes, is designed to capture all essential flow features, including the turbulent boundary layers on the surface of the body. Our results are in good agreement with measurements … Show more

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Cited by 90 publications
(100 citation statements)
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References 42 publications
(63 reference statements)
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“…The pressure Poisson equation is solved directly using fast Fourier transforms in the periodic directions (x 1 and x 3 ) and a tridiagonal matrix algorithm in the wall-normal direction (x 2 ). Beratlis, Balaras & Kiger (2007) and Posa & Balaras (2016) used the same solver with an immersed boundary formulation for treating complex geometries. A description of the numerical scheme along with a detailed validation can be found in Balaras (2004).…”
Section: Problem Formulation and Solution Methodsmentioning
confidence: 99%
“…The pressure Poisson equation is solved directly using fast Fourier transforms in the periodic directions (x 1 and x 3 ) and a tridiagonal matrix algorithm in the wall-normal direction (x 2 ). Beratlis, Balaras & Kiger (2007) and Posa & Balaras (2016) used the same solver with an immersed boundary formulation for treating complex geometries. A description of the numerical scheme along with a detailed validation can be found in Balaras (2004).…”
Section: Problem Formulation and Solution Methodsmentioning
confidence: 99%
“…The mean velocity profiles of the current simulation are in good agreement with the similarity law and the results in Refs. [25] and [27]. Fig.…”
Section: Distributions Of the Velocity And Pressurementioning
confidence: 98%
“…(25) are algebraic, and the wall shear stress can be reconstructed by the numerical integration of Eq. (25) under the boundary condition provided by the probe point in each time step.…”
Section: Implementation Of the Wall Modelsmentioning
confidence: 99%
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